Multi-variate assumed PDF modeling of turbulent sub- and supersonic combustion (English)
- New search for: Gerlinger, P.
- New search for: Schneider, F.
- New search for: Aigner, M.
- New search for: Gerlinger, P.
- New search for: Schneider, F.
- New search for: Aigner, M.
In:
ISABE, International Symposium on Air Breathing Engines, 18
;
1-12
;
2007
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ISBN:
- Conference paper / Storage medium
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Title:Multi-variate assumed PDF modeling of turbulent sub- and supersonic combustion
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Additional title:Multivariate Modellierung mit angenommener Wahrscheinlichkeitsdichte für tubulente Unter- und Überschallverbrennung
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Contributors:
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Published in:
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Publisher:
- New search for: American Institute of Aeronautics and Astronautics (AIAA)
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Place of publication:Reston
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Publication date:2007
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Size:12 Seiten, 18 Bilder, 2 Tabellen, 17 Quellen
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ISBN:
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Type of media:Conference paper
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Type of material:Storage medium
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Language:English
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Keywords:Gasdynamik , Verbrennung (Oxidation) , Überschallströmung , Unterschallströmung , Mach-Zahl , Überschallstaustrahltriebwerk , Wasserstoff , chemische Reaktion , Wahrscheinlichkeitsdichte , mathematisches Modell , Navier-Stokes-Gleichung , partielle Differenzialgleichung , Temperaturverteilung , Diskretisierung (Berechnung)
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Source:
Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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Design of a contra-rotating turbine for a hypersonic aircraftPaniagua, Guillermo / Szokol, Szabolcs / Kato, Hiromasa / Manzini, Giovanni / Varvill, Richard et al. | 2007
- 1
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Total temperature probes for turbine and combustor applicationsZeisberger, Andreas et al. | 2007
- 1
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AIAA-2007-1006 ROLLS-ROYCE - BRINGING TECHNOLOGY TO MARKETPrice, P.D. / American Institute of Aeronautics and Astronautics et al. | 2007
- 1
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Assessment of numerical methods on a 3.5-stage axial compressorWang, Zhuo / Niehuis, Reinhard et al. | 2007
- 1
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Investigation of the influence of streamwise vortices generating geometries of strut injectors on the mixing and combustion process in a scramjet model combustorScheel, Frithjof / Ciezki, Helmut K. / Haidn, Oskar J. et al. | 2007
- 1
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Experimental study of orifice discharge coefficients in high-speed rotating shaftsSousek, J. / Pfitzner, M. et al. | 2007
- 1
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Aero-thermal analysis of a partially shrouded axial turbinePorecca, L. / Kalfas, A.I. / Abhari, R.S. et al. | 2007
- 1
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Retrofit of a digital engine control unit and integration of an active stability control systemBindl, Stefan / Niehuis, Reinhard / Zähringer, Christian / Grauer, Frank et al. | 2007
- 1
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Adaptive machining technology and data management for automated repair of complex turbine components with focus on blisk repairBremer, Claus et al. | 2007
- 1
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Analysis of blade vibration in a blisk type turbine using non-intrusive stress measurement systemJoung, Kyukang / Kim, Jonggoo / Kim, Myungho / Kim, Yeongryeon et al. | 2007
- 1
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Laminar to turbulent transitional behaviour of the boundary layer obtained from high speed rig test results and 3D-navier-stokes calculation with transition modelJohann, E. / Swoboda, M. et al. | 2007
- 1
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Micro combustor for micro gas turbine enginesGuidez, Joel / Roux, Patrick / Poirson, Nicolas / Laurent, Corentin et al. | 2007
- 1
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Oil-free rotor support technologies for an optimized helicopter propulsion systemDellaCorte, Christopher / Bruckner, Robert J. et al. | 2007
- 1
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Design and validation of a real-time model for steady-state and transient performance simulation of a helicopter engineFrowein, J. von / Abdullahi, H. / Erhard, W. / Schmidt, K.J. et al. | 2007
- 1
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Multi-variate assumed PDF modeling of turbulent sub- and supersonic combustionGerlinger, P. / Schneider, F. / Aigner, M. et al. | 2007
- 1
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Desensitization of turbine flow field and performance from rotor tip gap using casing injectionBehr, Thomas / Kalfas, Anestis I. / Abhari, Reza S. et al. | 2007
- 1
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Effect of clocking on unsteady blade loading in a four-stage low-speed axial compressor Part 1: Numerical investigationJia, Huixia / Xi, Guang / Müller, Lutz / Mailach, Ronald / Vogeler, Konrad et al. | 2007
- 1
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Flow study of a redesigned high pressure ratio centrifugal compressorKrain, H. / Hoffmann, B. et al. | 2007
- 1
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Ultra lightweight ducted fan propulsion unit for light aircraftHanus, Daniel / Censky, Tomas et al. | 2007
- 1
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Experimental investigation of flow and mixing in a gas turbine combustor modelFindeisen, Jens / Schiffer, H. -P. et al. | 2007
- 1
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Recent progress in the hybrid-grid CFD simulation of turbomachinery flowsYang, Hong / Nuernberger, Dirk / Kuegeler, Edmund et al. | 2007
- 1
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Alternate fuels for use in commercial aircraftDaggett, David L. / Hendricks, Robert C. / Walther, Rainer / Corporan, Edwin et al. | 2007
- 1
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Notch sensitivity and intergranular crack growth in the Allvac 718Plus superalloyAndersson, Joel / Sjöberg, Göran / Hatami, Sepehr et al. | 2007
- 1
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Experimental investigation of rotating stall in a research multistage axial compressorLepicovsky, Jan et al. | 2007
- 1
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Rotating instability in a transonic compressorHah, Chunill / Bergner, Jörg / Schiffer, Heinz-Peter et al. | 2007
- 2
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AIAA-2007-1008 PRIORITY SCIENTIFIC RESEARCHES IN CIAM FOR MODERN AIRCRAFT ENGINE DEVELOPMENTSkibin, V.A. / American Institute of Aeronautics and Astronautics et al. | 2007
- 3
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AIAA-2007-1010 AN OVERVIEW OF JAXA'S TECHCLEAN PROJECT - TECHNOLOGY DEVELOPMENT PROJECT FOR ENVIRONMENTALLY COMPATIBLE AEROENGINESHayashi, S. / American Institute of Aeronautics and Astronautics et al. | 2007
- 5
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AIAA-2007-1101 ADAPTIVE MACHINING TECHNOLOGY AND DATA MANAGEMENT FOR AUTOMATED REPAIR OF COMPLEX TURBINE COMPONENTS WITH FOCUS ON BLISK REPAIRBremer, C. / American Institute of Aeronautics and Astronautics et al. | 2007
- 6
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AIAA-2007-1102 PHASES OF A HIGH-TECH REPAIR IMPLEMENTATION, DEFINITION, DEVELOPMENT, ADAPTATION, VALIDATION AND QUALIFICATION, IN CASE OF PATCH-REPAIR ON BLISK-BLADESEberlein, A. / American Institute of Aeronautics and Astronautics et al. | 2007
- 8
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AIAA-2007-1103 ARCHITECTURE OF A TECHNO-ECONOMIC AND ENVIRONMENTAL RISK ASSESSMENT TOOL USING A MULTI-MODULAR BUILD APPROACHBretschneider, S. / Staudacher, S. / Arago, O. / American Institute of Aeronautics and Astronautics et al. | 2007
- 9
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AIAA-2007-1105 MINIMIZING DIRECT OPERATING COSTS (DOC) FOR A SMALL EUROPEAN AIRLINEEkstrand, H. / Avellan, R. / Gronstedt, T. / American Institute of Aeronautics and Astronautics et al. | 2007
- 10
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AIAA-2007-1106 OPERATING COST AND RISK ANALYSIS FOR AIRCRAFT AND ENGINESPascovici, D. / Colmenares, F. / Ogaji, S. / Suria, O.V. / Pilidis, P. / American Institute of Aeronautics and Astronautics et al. | 2007
- 15
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AIAA-2007-1107 ANALYSIS OF BLADE VIBRATION IN A BLISK TYPE TURBINE USING NON-INTRUSIVE STRESS MEASUREMENT SYSTEMJoung, K. / Kim, J. / Kim, M. / Kim, Y. / American Institute of Aeronautics and Astronautics et al. | 2007
- 17
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AIAA-2007-1108 TOTAL TEMPERATURE PROBES FOR TURBINE AND COMBUSTOR APPLICATIONSZeisberger, A. / American Institute of Aeronautics and Astronautics et al. | 2007
- 19
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AIAA-2007-1109 NONCONTACT BLADE VIBRATION AND TIP CLEARANCE MEASUREMENT SYSTEM FOR AERO ENGINE APPLICATIONZielinski, M. / Ziller, G. / American Institute of Aeronautics and Astronautics et al. | 2007
- 20
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AIAA-2007-1110 EFFECT OF T56 PRESWIRL COOLING MODELLING ON DISC ASSEMBLY TEMPERATURE PREDICTIONRoos, T. / Kruger, E. / American Institute of Aeronautics and Astronautics et al. | 2007
- 21
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AIAA-2007-1111 HIGH-TEMPERATURE RESISTANT PRESSURE TRANSDUCER FOR MONITORING OF GAS TURBINE COMBUSTION STABILITYGiuliani, F. / Schricker, A. / Lang, A. / Leitgeb, T. / Heitmeir, F. / American Institute of Aeronautics and Astronautics et al. | 2007
- 23
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AIAA-2007-1113 RESEARCH OF A PRECONDITIONED ROE SCHEME FOR ALL SPEED FLOWS IN TURBOMACHINERYLi, X. / Gu, C.-w. / Xu, J.-z. / American Institute of Aeronautics and Astronautics et al. | 2007
- 24
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AIAA-2007-1116 AN AERODYNAMIC ASSESSMENT OF MANUFACTURING DEFECTS THROUGH ROBUST DESIGNNilsson, M. / Fredrik, W. / American Institute of Aeronautics and Astronautics et al. | 2007
- 25
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AIAA-2007-1117 MULTIPLE POINT ADAPTIVE PERFORMANCE SIMULATION TUNED TO AERO-ENGINE TEST BED DATAMarinai, L. / Li, Y.-G. / Pachidis, V. / American Institute of Aeronautics and Astronautics et al. | 2007
- 26
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AIAA-2007-1118 VITAL - EUROPEAN R&D PROGRAMME FOR GREENER AERO-ENGINESKorsia, J.-J. / American Institute of Aeronautics and Astronautics et al. | 2007
- 28
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AIAA-2007-1120 NEW ENVIRONMENTAL FRIENDLY AERO ENGINE CORE CONCEPTSWilfert, G. / Sieber, J. / Rolt, A. / Touyeras, A. / Baker, N. / American Institute of Aeronautics and Astronautics et al. | 2007
- 30
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AIAA-2007-1121 EFFECTS OF AERODYNAMIC TABS ON NOISE REDUCTION OF A RECTANGULAR PLUG NOZZLEAraki, M. / Shiga, S. / Kojima, T. / Taguchi, H. / American Institute of Aeronautics and Astronautics et al. | 2007
- 31
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AIAA-2007-1123 LOW NOISE RESEARCH AND DEVELOPMENT IN JAPANESE ENVIRONMENTALLY COMPATIBLE ENGINE FOR SMALL AIRCRAFT PROJECTOishi, T. / Yamane, T. / Oba, Y. / Ogawara, K. / American Institute of Aeronautics and Astronautics et al. | 2007
- 32
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AIAA-2007-1125 DESIGN AND VALIDATION OF A REAL-TIME MODEL FOR STEADY-STATE AND TRANSIENT PERFORMANCE SIMULATION OF A HELICOPTER ENGINEFrowein, J. / Abdullahi, H. / Erhard, W. / Schmidt, K.-J. / American Institute of Aeronautics and Astronautics et al. | 2007
- 33
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AIAA-2007-1126 TOWARD AN EFFICIENT AND SILENT ENGINE INTEGRATION ON A HELICOPTERBaude, P. / Clary, E. / Biscay, P. / Regaud, P.L. / American Institute of Aeronautics and Astronautics et al. | 2007
- 34
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AIAA-2007-1127 GAS TURBINE TECHNOLOGY FOR UNMANNED AIR VEHICLESBradbrook, S.J. / American Institute of Aeronautics and Astronautics et al. | 2007
- 35
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AIAA-2007-1128 MULTI-FUEL WANKEL ENGINE FOR SMALL AIRCRAFTS AND UAVS APPLICATION: STRATEGIES OF THE ENGINE DEVELOPMENTPoojitganont, T. / Berg, H.P. / Izweik, H.T. / Himmelberg, A. / American Institute of Aeronautics and Astronautics et al. | 2007
- 36
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AIAA-2007-1129 ULTRA-LIGHTWEIGHT DUCTED FAN PROPULSION UNIT FOR LIGHT AIRCRAFTHanus, D. / Censky, T. / American Institute of Aeronautics and Astronautics et al. | 2007
- 37
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AIAA-2007-1130 DEVELOPMENT AND FLIGHT-TESTING OF A SOLID FUEL RAMJET VEHICLEGany, A. / American Institute of Aeronautics and Astronautics et al. | 2007
- 38
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AIAA-2007-1131 RESEARCH TRAINING GROUP GRK 1095/1: AERO-THERMODYNAMICAL DESIGN OF A SCRAMJET PROPULSION SYSTEMGaisbauer, U. / Weigand, B. / Reinartz, B. / American Institute of Aeronautics and Astronautics et al. | 2007
- 39
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AIAA-2007-1132 TIP-TO-END AIR SIMULATION OF AIRFRAME INTEGRATED SCRAMJET ENGINERajinikanth, B. / Anavaradham, T.K.G. / American Institute of Aeronautics and Astronautics et al. | 2007
- 40
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AIAA-2007-1133 INVESTIGATION OF MODEL SCRAMJET PERFORMANCEChen, L. / Gu, H. / Xiao, Y. / Chan, X. / American Institute of Aeronautics and Astronautics et al. | 2007
- 42
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AIAA-2007-1134 EXPERIMENT STUDY OF SHOCK TRAIN IN A SCRAMJET ISOLATORWang, C. / Zhang, K.-Y. / Zhou, C. / Sun, B. / Cao, X.-b. / American Institute of Aeronautics and Astronautics et al. | 2007
- 43
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AIAA-2007-1135 CLUSTERED ROCKET CHAMBER FOR ROCKET-RAMJET COMBINED CYCLE ENGINETakegoshi, M. / Tomioka, S. / Ueda, S. / Saito, T. / American Institute of Aeronautics and Astronautics et al. | 2007
- 44
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AIAA-2007-1136 DESIGN AND DEVELOPMENT OF ADVANCED TRANSONIC FAN ROTORMurooka, T. / Goto, S. / Mizuta, I. / Kodama, H. / American Institute of Aeronautics and Astronautics et al. | 2007
- 45
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AIAA-2007-1137 DESIGN AND PERFORMANCE OF A FRONT STAGE AND FOR A HIGH PRESSURE RATIO FAN DEMONSTRATORMartensson, H. / Burman, J. / Lundh, C. / Johansson, U. / American Institute of Aeronautics and Astronautics et al. | 2007
- 46
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AIAA-2007-1138 NUMERICAL AND EXPERIMENTAL INVESTIGATION OF BYPASS FANSMileshin, V. / American Institute of Aeronautics and Astronautics et al. | 2007
- 47
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AIAA-2007-1139 DESIGN AND NUMERICAL INVESTIGATION OF A HIGH-PRESSURE RATIO COUNTER-ROTATING FANXi-Yang, L. / Zhao, X. / American Institute of Aeronautics and Astronautics et al. | 2007
- 48
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AIAA-2007-1140 IMPACT OF COMPLEX SWIRL PATTERNS ON COMPRESSOR PERFORMANCE AND OPERABILITY USING PARALLEL COMPRESSOR ANALYSISBouldin, B. / Sheoran, Y. / American Institute of Aeronautics and Astronautics et al. | 2007
- 49
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AIAA-2007-1141 FAN-INLET FLOW-FIELD COUPLINGHunes, T.P. / Athayde, P.A.V. / American Institute of Aeronautics and Astronautics et al. | 2007
- 50
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AIAA-2007-1142 ASSESSMENT OF FUTURE AIRCRAFT TECHNOLOGIES ON ENGINE NOISE AND FUEL CONSUMPTIONHall, C.A. / Schwartz, E. / American Institute of Aeronautics and Astronautics et al. | 2007
- 51
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AIAA-2007-1143 DISCUSSION OF MODELS FOR AERO-ENGINE BUSINESS COOPERATION (BETWEEN CHINA AND OTHER COUNTRIES)Zhang, S. / Kelly, J. / American Institute of Aeronautics and Astronautics et al. | 2007
- 52
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AIAA-2007-1144 SIMULATION ENVIRONMENT FOR THE VIRTUAL DEVELOPMENT AND TESTING OF PROPULSION SYSTEMSLavelle, T. / Lytle, J.K. / Horowitz, J. / American Institute of Aeronautics and Astronautics et al. | 2007
- 53
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AIAA-2007-1145 OIL-FREE ROTOR SUPPORT TECHNOLOGIES FOR AN OPTIMIZED HELICOPTER PROPULSION SYSTEMDellaCorte, C. / Bruckner, R.J. / American Institute of Aeronautics and Astronautics et al. | 2007
- 54
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AIAA-2007-1146 ADVANCED OIL SYSTEM ARCHITECTURES AND COMPONENTSRaimaeckers, N. / Saive, G. / American Institute of Aeronautics and Astronautics et al. | 2007
- 55
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AIAA-2007-1149 ON THE TRADE OFF BETWEEN CO2 AND CONTRAILSNoppel, F.G. / Singh, R. / American Institute of Aeronautics and Astronautics et al. | 2007
- 56
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AIAA-2007-1150 THE AVOIDANCE OF CONTRAILS BY ADVANCED TECHNICAL MEANSNoppel, F.G. / Singh, R. / American Institute of Aeronautics and Astronautics et al. | 2007
- 57
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AIAA-2007-1151 ENGINE NOISE RESEARCH IN NASA'S QUIET AIRCRAFT TECHNOLOGY PROJECTGrady, J.E. / Weir, D.S. / Lamoureux, M.C. / Martinez, M.M. / Envia, E. / Bridges, J.E. / Huff, D.L. / American Institute of Aeronautics and Astronautics et al. | 2007
- 58
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AIAA-2007-1153 HIGH FIDELITY SYSTEM SIMULATION OF A GAS TURBINE ENGINEClaus, R. / Townsend, S. / Lavelle, T. / Turner, M. / American Institute of Aeronautics and Astronautics et al. | 2007
- 59
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AIAA-2007-1154 ADVANCED CYCLES FOR DISTRIBUTED PROPULSIONAmeyugo, G. / Singh, R. / American Institute of Aeronautics and Astronautics et al. | 2007
- 60
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AIAA-2007-1156 POTENTIAL OF VARIABLE CYCLE ENGINES FOR SUBSONIC AIR TRANSPORTLundblach, A. / Avellan, R. / American Institute of Aeronautics and Astronautics et al. | 2007
- 61
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AIAA-2007-1157 MISSION OPTIMIZATION OF AN INTERCOOLED TURBOFAN ENGINELei, X. / Gustafsson, B. / Gronstedt, T. / American Institute of Aeronautics and Astronautics et al. | 2007
- 62
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AIAA-2007-1159 AN OPPORTUNITY FOR CREATION OF HIGHLY EFFECTIVE AVIATION AUXILLARY POWER PLANTS WITH GAS-STEAM-TURBINE CONTOURYanovskiy, L.S. / Baykov, A.V. / American Institute of Aeronautics and Astronautics et al. | 2007
- 63
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AIAA-2007-1161 RECENT PROGRESS IN THE RESEARCH ON ADVANCED COOLING TECHNOLOGIES FOR A NEXT-GENERATION AERO-ENGINEOkita, Y. / Fukuyama, Y. / Nakamata, C. / Yoshida, T. / American Institute of Aeronautics and Astronautics et al. | 2007
- 65
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AIAA-2007-1162 SENSITIVITY ANALYSIS FOR HIGH PRESSURE TURBINE NOZZLE GUIDE VANE TEMPERATURE PREDICTIONRavitej, M. / Kesavan, V. / American Institute of Aeronautics and Astronautics et al. | 2007
- 66
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AIAA-2007-1164 3D FLOW STRUCTURES ADJACENT RECTANGULAR COOLING HOLESKang, S. / American Institute of Aeronautics and Astronautics et al. | 2007
- 67
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AIAA-2007-1165 HEAT TRANSFER CHARACTERISTICS OF A MULTI-STAGE COOLING SCHEME FOR GAS TURBINE ENGINESGhorab, M. / Hassan, I. / American Institute of Aeronautics and Astronautics et al. | 2007
- 68
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AIAA-2007-1166 DEVELOPMENT OF DIFFUSER PASSAGE COMPRESSOR CONCEPT FOR SMALL AIRCRAFT ENGINESKato, D. / Yamagami, M. / Kodama, H. / Outa, E. / American Institute of Aeronautics and Astronautics et al. | 2007
- 69
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AIAA-2007-1167 ISSUES FOR DEVELOPING ULTRA-MICRO COMBUSTORS FOR UMGT: HEAT LOSS, COMBUSTION METHOD AND FUELSaburo, Y. / Takashi, S. / Shoko, S. / Fong, W.S. / American Institute of Aeronautics and Astronautics et al. | 2007
- 70
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AIAA-2007-1168 EXPERIMENTAL SETTING EFFECTS ON MICRO WAVE ROTOR OPERATIONOkamoto, K. / Yamaguchi, K. / Nagashima, T. / American Institute of Aeronautics and Astronautics et al. | 2007
- 71
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AIAA-2007-1169 MICRO COMBUSTOR FOR MICRO GAS TURBINE ENGINEGuidez, J. / Roux, P. / Poirson, N. / Laurent, C. / American Institute of Aeronautics and Astronautics et al. | 2007
- 72
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AIAA-2007-1170 DEVELOPMENT OF A COMBUSTION CHAMBER FOR AN ULTRA MICRO GAS TURBINETrilla, J. / Becret, P. / Grossen, J. / Hendrick, P. / American Institute of Aeronautics and Astronautics et al. | 2007
- 73
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AIAA-2007-1171 STUDY ON HEAT TRANSFER AND STRESS OF A 100KW MICROTURBINE TEST RIG ROTOR CONSIDERING THE EFFECT OF 3-D THERMAL ELASTIC CONTACTXie, Y.-H. / Liu, X.-z. / Deng, Q.-H. / Feng, Z.-P. / American Institute of Aeronautics and Astronautics et al. | 2007
- 74
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AIAA-2007-1172 TURBULENT REACTING FLOW SIMULATIONS OF A WHOLE SCRAMJET ENGINE ON HYBRID/UNSTRUCTURED GRIDWang, L. / Wu, y. / Le, J. / American Institute of Aeronautics and Astronautics et al. | 2007
- 75
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AIAA-2007-1173 PERFORMANCE OF HYDROGEN-FUELLED VITIATED AIR HEATER FOR SUPERSONIC COMBUSTION STUDIESSatya, V. / Chandrasekhar, C. / Ramanujachari, V. / Panneerselvam, S. / American Institute of Aeronautics and Astronautics et al. | 2007
- 76
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AIAA-2007-1174 EFFECTS OF LIQUID FUEL PROPERTIES ON SUPERSONIC COMBUSTIONHashimoto, S. / Kazami, H. / Tsue, M. / Kono, M. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1175 EXPERIMENTAL INVESTIGATION OF STRUT BASED SUPERSONIC COMBUSTOR BURNING HYDROCARBON FUELChandrasekhar, C. / Tripath, D.K. / Ramanujachari, V. / Panneerselvam, S. / American Institute of Aeronautics and Astronautics et al. | 2007
- 78
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AIAA-2007-1176 TESTING METALLIZED SOLID FUEL SCRAMJET COMBUSTORGany, A. / American Institute of Aeronautics and Astronautics et al. | 2007
- 79
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AIAA-2007-1177 THEORETICAL MODELING OF THE COMBUSTION OF ORGANIC-GELLANT-BASED GEL FUEL DROPLETSKunin, A. / American Institute of Aeronautics and Astronautics et al. | 2007
- 80
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AIAA-2007-1178 VALIDATION OF STEADY AVERAGE-PASSAGE AND MIXING-PLANE CFD APPROACHES FOR THE PERFORMANCE PREDICTION OF A MODERN GAS TURBINE MULTISTAGE AXIAL COMPRESSORMansour, M.L. / Hayes, J.M. / Ramachandran, V. / Goswami, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1179 EFFECT OF TIP BALANCE ON THE FLOW STRUCTURE AND INTEGRAL PERFORMANCE OF A SIX-STAGE HPCMileshin, V. / Orekhov, I.K. / Fateyev, V.A. / Shchipin, S.K. / American Institute of Aeronautics and Astronautics et al. | 2007
- 83
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AIAA-2007-1180 FORCED RESPONSE PREDICTION SYSTEM FOR MULTI-STAGE COMPRESSOR BLADES/VANESSoda, Y. / Tsuchiya, N. / Asaumi, N. / Kato, D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1181 EFFECT OF CLOCKING ON UNSTEADY BLADE LOADING IN A FOUR-STAGE LOW-SPEED AXIAL COMPRESSOR. PART 1:NUMERICAL INVESTIGATIONJia, H. / Xi, G. / Muller, L. / Mailach, R. / Vogeler, K. / American Institute of Aeronautics and Astronautics et al. | 2007
- 85
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AIAA-2007-1182 EFFECT OF CLOCKING ON UNSTEADY BLADE LOADING IN A FOUR-STAGE LOW-SPEED AXIAL COMPRESSOR. PART 2:EXPERIMENTAL INVESTIGATIONXi, G. / Jia, H. / Muller, L. / Mailach, R. / Vogler, K. / American Institute of Aeronautics and Astronautics et al. | 2007
- 86
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AIAA-2007-1183 TURBULENCE MODELLING EFFECTS ON OFF-DESIGN PREDICTIONS FOR A MULTI-STAGE COMPRESSORSharma, V. / Schvallinger, M. / Marty, J. / Gaible, H. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1184 DESIGN AND TEST DEMONSTRATION OF THE JET01 SIX STAGE HIGH PRESSURE COMPRESSORCheng, R. / Wenger, U. / Faxiang, L. / Tian, X. / American Institute of Aeronautics and Astronautics et al. | 2007
- 88
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AIAA-2007-1185 EXPERIMENTAL INVESTIGATION OF THE PATTERN FACTOR AND LBO OF HIGH TEMPERATURE RISE COMBUSTORXu, Q. / Peng, Y. / Lin, Y. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1186 PRANDTL/SCHMIDT NUMBER EFFECT ON TEMPERATURE DISTRIBUTION IN A MODEL COMBUSTORJiang, L. / Campbell, I. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1187 TIME-RESOLVED ANALYSIS OF DENSITY FLUCTUATIONS IN A RESONANT AIR-METHANE FLAME USING DUAL LASER VIBROMETRY FOR GAS TURBINE COMBUSTOR QUALIFICATION TESTSGiuliani, F. / Lang, A. / Leitgeb, T. / Woisetschlager, J. / Heitmeir, F. / American Institute of Aeronautics and Astronautics et al. | 2007
- 91
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AIAA-2007-1188 TOWARDS LES OF MIXING PROCESSES INSIDE A RESEARCH RAMJET COMBUSTORReichstadt, S. / Bertier, N. / Ristori, A. / Bruel, P. / American Institute of Aeronautics and Astronautics et al. | 2007
- 92
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AIAA-2007-1189 A COMPUTATIONAL STUDY FOR NON-REACTING FLOW OF SIDE-DUMP COMBUSTOR USING LARGE-EDDY SIMULATIONChen, J. / Zheng, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1190 LOW NOX COMBUSTOR DEVELOPMENT FOR THE ENGINE3E CORE ENGINE DEMONSTRATORLazik, W. / Doerr, T. / Bake, S. / American Institute of Aeronautics and Astronautics et al. | 2007
- 94
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AIAA-2007-1191 CONTINUOUS OPERATION OF A CYLINDRICAL ROTARY VALVE PDE AT A LOW SUPPLY PRESSURE CONDITIONMotohide, M. / Takashi, S. / Satoshi, Y. / Shigeharu, O. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1192 ANALYSIS OF AN AIR-BREATHING PULSED DETONATION ENGINE WITH BYPASS AND EJECTOR CONCEPTCha, X. / Chuan-jun, Y. / Hua, Q. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1194 A PRELIMINARY FEASIBILITY STUDY FOR FUTURE AERO ENGINESColmenares, F. / Gomez, J. / Pascovici, D. / Ogaji, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1195 PRELIMINARY DESIGN OF SUBSONIC TRANSPORT AIRCRAFT / ENGINESAvellan, R. / Gronstedt, T. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1196 ALTERNATE FUELS FOR USE IN FUTURE COMMERCIAL AIRCRAFTCorporan, E. / Daggett, D.L. / Hendricks, R.C. / Walther, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1198 ASSESSMENT OF COMPETING CFD TURBULENCE AND GRID MODELS IN PREDICTING DISK CAVITY HEAT TRANSFER AND FRICTION RESISTANCEHo, K.-S. / Yang, Y.-Q. / Reyes, V. / Jeff, H. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1199 DEVELOPMENT OF AN EFFUSION-COOLED COMBUSTOR FOR THE TFE731 TURBOFAN ENGINEDudebout, R. / Bohman, R. / Reynolds, B. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1200 PREDICTING TURBOMACHINERY BLADE COOLING BY AN IMMERSED BOUNDARY METHODDe Palma, P. / de Tullio, M.D. / Pascazio, G. / Napolitano, M. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1201 AN EXPERIMENTAL STUDY ON LOCAL HEAT TRANSFER ENHANCEMENT BY IMPINGEMENT IN A COMBUSTOR LINER RESONATORXing, Y. / Lauffer, D. / Weigand, B. / von Wolfersdorf, J. / Dahlke, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1203 AERO-PROPULSIVE PERFORMANCE FOR VEHICLE MODEL WITH CFD AND EXPERIMENTSLe, J. / Weixiong, L. / Wei, H. / Yuanyuan, H. / Zhonghua, Z. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1204 PRELIMINARY DEFINITION OF A TBCC PROPULSION SYSTEM FOR A MACH 4.5 SUPERSONIC CRUISE AIRLINERSippel, M. / Okai, K. / Kumar, A. / Kato, H. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1205 LAPCAT: A TECHNICAL FEASIBILITY STUDY ON SUSTAINED HYPERSONIC FLIGHTSteelant, J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1208 NASA HYPERSONIC PROPULSION - OVERVIEW OF PROGRESS FROM 1995 TO 2005Cikanek, H.A. / Bartolotta, P.A. / Klem, M.D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1209 A QUANTITATIVE STUDY OF INLET GROUND VORTICESMurphy, J.P. / Taylor, M.D. / MacManus, D.G. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1210 NUMERICAL SIMULATION OF THE DISTORTION GENERATED BY CROSSWIND INLET FLOWSColin, Y. / Aupoix, B. / Boussuge, J.F. / Chanez, P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1211 EXPERIMENTAL STUDY ON THE SUPERSONIC INLET BUZZ WITH ANGLE OF ATTACKLee, H.J. / Kim, S.D. / Jeung, I.-S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1212 NUMERICAL AND EXPERIMENTAL INVESTIGATIONS FOR SUPERSONIC INVERTED INLETZhu, S. / Cui, D. / Zheng, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1213 OPTIMUM DESIGN OF A SUPERSONIC BUMP-TYPE INLETSong, D.J. / Kim, S.D. / Lim, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1215 A QUASI-ONE-DIMENSIONAL MODEL FOR AXIAL TURBINESAdam, O. / Leonard, O. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1216 NUMERICAL INVESTIGATION OF TURBINE CASCADE WITH HIGH OUTLET MACH NUMBERXiang, X. / Zhao, X. / Xu, J.-z. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1217 EXPERIMENTAL AND NUMERICAL INVESTIGATIONS ON THE AERODYNAMIC PERFORMANCE OF THE FORE-LOADED AND AFT-LOADED TURBINE BLADESLi, J. / Sun, Q. / Wang, J.-l. / Feng, Z.-P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1218 UNSTEADY STRONG SHOCKS INTERACTIONS IN A TRANSONIC TURBINE: EXPERIMENTAL AND NUMERICAL ANALYSISPaniagua, G. / Yasa, T. / de la Loma, A. / Castillon, L. / Colon, T. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1220 PERFORMANCE IMPROVEMENT OF HP AND LP TURBINE IN ECO ENGINETanimitsu, H. / Hamazaki, H. / Mitsuhashi, K. / Asaumi, N. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1221 DESENSITIZATION OF TURBINE FLOW FIELD AND PERFORMANCE FROM ROTOR TIP GAP USING CASING INJECTIONBehr, T. / Kalfas, A.I. / Abhari, R.S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1223 FLOW STUDY OF A REDESIGNED HIGH PRESSURE RATIO CENTRIFUGAL COMPRESSORKrain, H. / Hoffmann, B. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1224 INVESTIGATION OF FLOW FIELD PERFORMANCE AND OPTIMIZING ADJUSTING TECHNOLOGIES OF AXIAL-CENTRIFUGAL COMPRESSORChen, Y. / Liu, B. / Xiang, X. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1225 EFFECT OF LEADING EDGE SWEEP ON PERFORMANCE OF A TRANSONIC CENTRIFUGAL IMPELLERHazby, H.R. / Xu, L. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1226 EFFECT OF IMPELLER-DIFFUSER INTERACTION ON CENTRIFUGAL COMPRESSOR PERFORMANCEGogoi, A. / Prakash, D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1227 NUMERICAL INVESTIGATION OF THE INTERACTION BETWEEN THE IMPELLER AND DIFFUSERChu, L. / Du, J. / Zhao, X. / Xu, J.-z. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1229 ON UNIQUENESS OF INVERSE PROBLEM SOLUTION OF COMPRESSIBLE FLOW ALONG AN ARBITRARY STREAM SHEET OF REVOLUTION: (I) CHANNEL DESIGNLiu, G.-L. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1230 NUMERICAL SIMULATIONS OF FLUID-STRUCTURE INTERACTIONS USING IMMERSED BOUNDARY METHODZhong, G. / Sun, X. / Liang, A. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1231 RECENT PROGRESS IN THE HYBRID-GRID CFD SIMULATION OF TURBOMACHINERY FLOWSYang, H. / Dick, N. / Kuegeler, E. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1233 DIRECT CALCULATION OF AERODYNAMIC INFLUENCE COEFFICIENTS USING A COMMERCIAL CFD SOLVERVogt, D.M. / Martensson, H.E. / Fransson, T.H. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1234 NUMERICAL SIMULATION ON SPRAY COMBUSTION FLOWS IN DUMP TYPE RAMJET COMBUSTORKim, S.D. / Jeung, I.-S. / Choi, J.-Y. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1235 EFFECTS OF HEAT ADDITION AND DUCT DIVERGENCE ON PSEUDO-SHOCK WAVESChoi, B. / Goto, M. / Mizushima, H. / Masuya, G. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1236 PROBLEMS OF THE METHANE-CONTAINING SUPERSONIC BLOCK-JET COMBUSTION ORGANIZATION UNDER TURBULENT MIXING WITH A WAKE SUBSONIC AIR FLOW IN THE COMBUSTION CHAMBER OF A ROCKET RAMJET ENGINETimoshenko, V. / Belotserkovets, I.S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1238 EXPERIMENTAL RESEARCH ON SUPERSONIC COMBUSTION IN RESISTANCE HEATED FACILITYSong, W. / Wang, D. / Zhong, Z. / Jialing, L. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1240 ADVANCED HEAT EXCHANGERS FOR USE WITH AIRCRAFT ENGINESStrumpf, H.J. / Muley, A. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1242 DESIGN OF THE QUALIFICATION TEST FACILITY AND ENDURANCE TEST FOR COMPACT HEAT EXCHANGERSBhaskar, A.C. / Ranganayakulu, C. / Vizhian, S.P. / Rao, T.M. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1243 NUMERICAL PREDICTION OF THE MINIMUM PURGE FLOW REQUIRED TO SEAL ROTOR-STATOR CAVITIES AGAINST HOT GAS INGESTIONSchwientek, A. / Chehab, E. / von Wolfersdorf, J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1246 RESEARCH ON THREE DIMENSIONAL COMPRESSION SCRAMJET INLETYabin, X. / Lian-Jie, Y. / Peng, G. / Xin-Yu, C. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1247 ANALYSIS OF ADDITIVE DRAG IN SIDEWALL-COMPRESSION INLETLuo, X.-C. / Zhang, K.-Y. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1248 CFD ANALYSIS OF MODULAR HYPERSONIC BUSEMANN INLETSSun, B. / Zhang, K.-Y. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1249 LARGE-EDDY SIMULATION OF SHOCK-WAVE/BOUNDARY LAYER INTERACTIONS IN HYPERSONIC INLET COMPRESSION RAMPSKrishnan, L. / Sandham, D. / Steelant, J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1250 IDENTIFICATION OF BLADE PASSING HARMONICS OF INDIVIDUAL WHEELS IN TURBINE ENGINESWang, W. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1251 RETROFIT OF A DIGITAL ENGINE CONTROL UNIT AND INTEGRATION OF AN ACTIVE STABILITY CONTROL SYSTEMBindl, S. / Niehuis, R. / Zahringer, C. / Graue, F. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1255 A STUDY OF ARTIFICIAL INTELLIGENT FAULT DETECTION OF PROPULSION SYSTEM FOR SMART UAVKong, C. / Ki, J. / Kho, S. / Lee, C. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1257 AN INVESTIGATION OF UNSTAEDY AERODYNAMIC LOAD ON TURBINE BLADE CONSIDERING ROTOR-STATOR INTERACTIONSXie, Y.-H. / Lan, J.-B. / Fan, T. / Zhang, D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1258 APPLICATION OF EDGE MATCHING TO MAXIMIZING THREE-DIMENSIONAL CLOCKING BENEFITJi, L.-C. / Yi, W. / Yan, Z. / Chen, J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1259 PULSED DETONATION ENGINE AND TURBINE INTERACTIONSTangirala, V.E. / Rasheed, A. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1260 THE ATTENUATION OF A DETONATION WAVE BY AN AIRCRAFT ENGINE AXIAL TURBINE STAGEVan Zante, D. / Envia, E. / Turner, M.G. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1261 PROBABILISTIC STUDY OF A TURBINE BLADEGorla, R.S.R. / Agrawal, V. / Murthy, P. / Venkataraman, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1262 ROTATING INSTABILITY IN A TRANSONIC COMPRESSOR ROTORHah, C. / Bergner, J. / Schiffer, H.-P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1263 EXPERIMENTAL INVESTIGATION OF ROTATING STALL IN A RESEARCH MULTISTAGE AXIAL COMPRESSORLepicovsky, J. / Braunscheidel, E.P. / Welch, G.E. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1265 COMPARISON OF AXIAL FLOW COMPRESSOR STALL PREDICTION CRITERIAvon Backstrom, T.W. / Gill, A. / Thiar, G.D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1266 THE ANALYSIS OF THE STALL PROCESS OF A TRANSONIC COMPRESSORFu, S. / Huang, X. / Chen, H. / Wadia, A.R. / Wisler, D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1267 EXPERIMENTAL STUDY OF STABILITY IMPROVEMENT BY TIP INJECTION AT MID CHORD REGION OF AXIAL COMPRESSORRoy, B. / Kaundinya, K.V. / Chouhan, M. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1268 COMPREHENSIVE COMBUSTION MODELING AND SIMULATION: RECENT PROGRESS AT NASA GLENN RESEARCH CENTERLiu, N.-S. / Shih, T.-H. / Wey, T. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1269 INVESTIGATION OF METAL NANOPARTICLES IN AIRBREATHING COMBUSTIONYoung, G. / Balar, R. / Yu, K. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1270 HIGH PRESSURE LOW NOX EMISSIONS RESEARCH: RECENT PROGRESS AT NASA GLENN RESEARCH CENTERLee, C.-M. / Tacina, K.M. / Wey, C. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1271 EXPERIMENTAL INVESTIGATION OF FLOW AND MIXING IN A GAS TURBINE COMBUSTOR MODELFindeisen, J. / Schiffer, H.-P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1272 COMBUSTION DYNAMICS IN A MODEL GAS TURBINE WITH A SWIRL STABILIZED INJECTORSung, H.-G. / Yang, V. / Lee, D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1273 EVOLUTION OF TURBULENT STRUCTURE IN THE MODEL COMBUSTOR EQUIPPED WITH TURBULENCE RINGLee, C. / Rhee, I.S. / Yu, J. / Park, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1274 GAS TURBINE FAULT DIAGNOSIS USING DECISION FUSION WITH FUZZY APPROACHMathioudakis, K. / Kyriazis, A. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1275 COUPLING PRINCIPAL COMPONENT ANALYSIS AND KALMAN FILTER ALGORITHMS FOR ON-LINE AIRCRAFT ENGINE DIAGNOSTICSBorguet, S. / Leonard, O. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1276 DETECTION OF CIRCUMFERENTIAL GAS TEMPERATURE DISTRIBUTION DISTORTION IN TIME/SPECTRAL DOMAIN METRICS OF VIBRATIONAL SIGNALSlacik, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1277 GAS EMISSIONS ACQUIRED DURING THE AIRCRAFT PARTICLE EMISSION EXPERIMENT (APEX) SERIESWey, C. / Wey, C.C. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1279 IN-DEPTH AND SURFACE, TRANSIENT FLUX PREDICTIONS USING HEATING/COOLING RATE (DT/DT) SENSORS AND ADVANCED ENGINEERING ANALYSIS FOR AEROSPACE APPLICATIONSFrankel, J.I. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1280 OPTICAL MEASUREMENTS IN A COMBUSTOR USING A 9 POINT SWIRL-VENTURI FUEL INJECTORHicks, Y.R. / Anderson, R.D. / Locke, R.J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1281 NEW ENGINE OF ``IVCHENKO-PROGRESS'' STATE ENTERPRISE IN THE 21ST CENTURYGavryshenko, A.V. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1282 ADVANCED TECHNOLOGIES FOR NEXT GENERATION REGIONAL JETS - SURVEY OF RESEARCH ACTIVITIES AT MTU AERO ENGINESWaschka, W. / Rud, K. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1283 GP7000 : MTU'S AERO ENGINES' CONTRIBUTION IN A SUCCESSFULL PARTNERSHIPWeber, S. / Hackenberg, H.-P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1285 AN ASSESSMENT OF NASA AEROPROPULSION TECHNOLOGIES - A SYSTEM STUDYTong, M.T. / Jones, S.M. / Haller, W.J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1290 ON-WING DECISION SUPPORT FOR AERO-ENGINE LINE REPLACEABLE UNIT FAULT ISOLATIONMills, A.R. / Tanner, G. / Thompson, H. / Fleming, P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1291 INVESTIGATION FOR CONSTRUCTING AERO ENGINE OIL SYSTEM STEADY MODELQiang, Z. / Liu, B. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1292 QUALIFICATION OF INDIGENOUSLY DEVELOPED PLATINUM ALUMINIDE COATING FOR AERO-ENGINE COMPONENTSSakthivel, A. / Raju, T.R. / Vedaprakash, B.S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1293 NOTCH SENSITIVITY AND INTERGRANULAR CRACK GROWTH IN THE ALLVAC 718PLUS SUPERALLOYAndersson, J. / Sjoberg, G. / Hatami, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1294 ARE SHAPE MEMORY ALLOYS ABOUT TO COME OF AGE FOR GAS TURBINE APPLICATIONS?Webster, J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1297 EXPERIMENTAL AND CFD INVESTIGATIONS OF FLOW IN COOLED AXIAL HIGH PRESSURE TURBINEReznyk, S. / Kravchenko, I. / Khomylyev, S. / Varvaruk, P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1298 NUMERICAL SIMULATION OF THE UNSTEADY EFFECT OF UPSTREAM WAKES AND SHOCKS ON FILM-COOLING IN A 1+1/2 TURBINE STAGEZhou, Y. / Zhao, X. / Xu, J.-z. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1299 AERO-THERMAL ANALYSIS OF A PARTIALLY SHROUDED AXIAL TURBINEKalfas, A.I. / Porreca, L. / Abhari, R.S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1300 NON-AXISYMMETRIC ENDWALL SHAPE OPTIMIZATION OF AN INTERMEDIATE TURBINE DUCTWallin, F. / Eriksson, L.-E. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1301 MULTIPLE OBJECTIVE OPTIMIZATION OF AXIAL TURBOMACHINES BASED ON INVERSE METHODLarocca, F. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1302 AERODYNAMIC IMPROVEMENT OF LOW PRESSURE TURBINE USING 3D VISCOUS FLOW COMPUTATIONSMurthy, S.V.R. / Ganesh, R. / Krishnaiah, T.V. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1303 LAMINAR TO TURBULENT TRANSITIONAL BEHAVIOR OF THE BOUNDARY LAYER OBTAINED FROM HIGH SPEED RIG TEST RESULTS AND 3D NAVIER-STOKES CALCULATIONS PART 1: TEST RESULTSJohann, E. / Swoboda, M. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1305 ASSESSMENT OF NUMERICAL METHODS ON A 3.5 STAGE AXIAL COMPRESSORWang, Z. / Niehuis, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1306 ADVANCED COMPRESSOR DESIGN INCORPORATING REAL GEOMETRY FEATURESLapworth, B.L. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1307 NONLINEAR ROTOR WAKE/STATOR INTERACTION COMPUTATIONS WITH BLADE SEPARATIONOlausson, M. / Eriksson, L.-E. / Baralon, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1308 NUMERICAL STUDY OF THE EFFECT OF BOUNDARY LAYER SUCTION ON THE SUPERSONIC ROTOR PERFORMANCEYi-Nan, X. / Liu, B. / Jin, J. / Yong-chen, Y. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1309 A SIMPLE METHOD AND PARAMETER STUDIES FOR TIP LEAKAGE MIXING LOSSShao, W. / Ji, L.-C. / Cheng, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1310 SENSITIVITY ANALYSIS FOR THE HYSHOT GENERIC SUPERSONIC COMBUSTION CONFIGURATIONMack, A. / Steelant, J. / Martinez-Schramm, J. / Hannemann, K. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1312 EFFECT OF THE TURBULENT SCHMIDT ON SUPERSONIC REGIMEIngenito, A. / Bruno, C. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1314 NUMERICAL INVESTIGATION OF MIXING ENHANCEMENT BY LOBED STRUT INJECTORS IN TURBULENT REACTIVE SUPERSONIC FLOWKindler, M. / Gerlinger, P. / Aigner, M. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1315 MULTI-VARIATE ASSUMED PDF MODELING OF TURBULENT SUB- AND SUPERSONIC COMBUSTIONGerlinger, P. / Schneider, F. / Aigner, M. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1316 INVESTIGATION OF THE INFLUENCE OF STREAMWISE VORTICES GENERATING GEOMETRIES OF STRUT INJECTORS ON THE MIXING AND COMBUSTION BEHAVIOR IN A SCRAMJET MODEL COMBUSTORCiezki, H.K. / Scheel, F. / Haidn, O.J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1317 PREDICTION AND CONTROL OF COMBUSTION INSTABILITIES IN A SWIRL TYPE COMBUSTORLi, X. / Feng, Z.-P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1318 ANALYSIS OF AN EXHAUST NOZZLE PERFORMANCE INTEGRATED WITH CO-FLOW FLUIDIC THRUST-VECTORINGGhoreyshi, M. / Pilidis, P. / Yarf-Abbassy, S. / Smith, H. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1319 AN APPROACH TO PERFORMANCE SIMULATION OF VARIABLE CONFLUENCE TURBOFAN FOR FUTURE SUPERSONIC CIVIL AIRCRAFT IN MULTI FIDELITY DISTRIBUTED ENVIRONMENTKorovkin, V. / Makarov, V. / Galerneau, M. / Coat, P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1320 EJECTORS PULSATING PROCESSES INVESTIGATIONSlobodkina, F. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1322 LDA MEASUREMENTS OF HEATED AND UNHEATED UNDEREXPANDED JETS FROM AXISYMMETRIC CONVERGENT NOZZLESFeng, T. / McGuirk, J.J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1323 A MODEL FOR PREDICTION OF CORNER SEPARATIONJi, L.-C. / Cheng, R. / Yi, W. / Shao, W. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1325 EXPERIMENTAL STUDY OF ORIFICE DISCHARGE COEFFICIENTS IN HIGH-SPEED ROTATING SHAFTSou_ek, J. / Pfitzner, M. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1328 WALL MOUNTED CAVITIES WITH AFT WALL MODIFICATIONSKurian, J. / Kurian, M.C. / Ali, M. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1330 DEVELOPMENT AND VALIDATION OF A MODULAR GAS TURBINE ENGINE PERFORMANCE MODEL FOR THE ASSESSMENT OF ADVANCED ENGINE TECHNOLOGIESVerstraete, D. / Hendrick, P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1332 PREDICTION OF HEATSOAKAGE AND TIP CLEARANCE EFFECTS ON GAS TURBINE TRANSIENT PERFORMANCESThiriet, R. / Masson, F. / Bertin, Y. / Dorignac, E. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1333 PREDICTION OF MODEL GAS TURBINE AFTERBURNER PERFORMANCE USING CFDGanesan, S. / Kumar, S.K. / Shankar, V. / Ganesan, V. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1334 TECHNOLOGY STRATEGY OF AERO GAS TURBINE ENGINE IN INDIADas, S. / Rao, T.M. / Rao, D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1335 MICRO PRESSURE SENSOR FOR HIGH TEMPERATURE APPLICATIONSLeo, A. / Stiharu, I. / Bhat, R.B. / Moustapha, H. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1336 MORE INTELLIGENT GAS TURBINE ENGINESStiharu, I. / Horn, W. / Fpoertner, H. / Moustapha, H. / Rosenfeld, T. / Webster, J. / Rybarik, P. / Schadow, K. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1337 NEW MATERIAL FOR PRESSURE SENSOR: SICN CERAMICS DERIVED FROM POLYUREASILAZANE PRECURSORAndronenko, S. / Stiharu, I. / Packirisamy, M. / Moustapha, H. / Dionne, P. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1338 A RETRO-FIT CONTROL ARCHITECTURE TO MAINTAIN ENGINE PERFORMANCE WITH USAGEGarg, S. / Sowers, T.S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1339 INVESTIGATION OF HOT STREAK-TO-AIRFOIL COUNT RATIO EFFECTS IN HIGH PRESSURE STAGE OF VANELESS COUNTER-ROTATING TURBINEQingjun, Z. / Huishe, W. / Zhao, X. / Xu, J.-z. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1340 BASIC ANALYSIS OF VANELESS COUNTER-ROTATING TURBOMACHINERYJi, L.-C. / Yi, W. / Ke, H. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1341 DESIGN OF A COUNTER-ROTATING TURBINE FOR A HYPERSONIC AIRCRAFTPaniagua, G. / Szokol, S. / Kato, H. / Manzini, G. / Varvill, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1343 INFLUENCE OF VARIOUS CASING DESIGN OVER A BLADE ON A STAGE EFFICIENCYGranovskiy, A. / Kostege, M. / Krupa, V. / Rudenko, S. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1344 EFFECTS OF AXIAL GAP ON THE VANE-ROTOR INTERACTION IN A HP TURBINE STAGEPersico, G. / Persico, P. / Osnaghi, C. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1345 TURBOMACHINERY BLADE THREE-DIMENSIONAL AERODYNAMIC OPTIMIZATION DESIGNChen, B. / Xin, J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1346 AERODYNAMIC OPTIMIZATION DESIGN OF 3-DIMENSIONAL TURBINE CASCADE WITH NON-AXISYMETRIC HUB END-WALLXuelin, G. / Xin, J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1347 NEXT GENERATION BOOSTERLebas, C. / Hiernaux, S. / Brouckaert, J.-F. / Leopot, I. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1348 PRE-STALL MODAL INSTABILITIES IN A TRANSONIC COMPRESSOR ROTORGannon, A.J. / Hobson, G.V. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1349 FULL ANNULUS FLOW SIMULATIONS IN A TRANSONIC FAN WITH BIRD INGESTION DAMAGEVogiatzis, C. / Balasubramanian, R. / Muthuruj, S. / Ramakrishna, C. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1350 EFFECT OF DROPLET INGESTION CONDITIONS ON ICE ACCRETION IN TURBOFAN ENGINESHamed, A. / Das, K. / Basu, D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1351 NUMERICAL SIMULATION OF BLADE SLOTS IN A SUBSONIC COMPRESSOR AT CONDITIONS NEAR STALLGourdain, N. / Montagnac, M. / Boussuge, J.F. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1352 COMPRESSOR STABILITY MANAGEMENTWadia, A.R. / Dhingra, M. / Neumeier, Y. / Prasad, J.V.R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1353 FUEL-AIR MIXING BY COMPRESSION CORNER IN SUPERSONIC BOUNDARY LAYERObata, S. / Nishio, K. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1354 METHODS OF ACTIVATION OF BORON PARTICLES IGNITION AND COMBUSTIONRosenband, V. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1355 INVESTIGATION OF HYDROCARBON-FUEL IGNITION AND COMBUSTION IN SCRAMJET COMBUSTORWang, D. / Wenyan, S. / Chen, I. / Cai, y. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1356 DYNAMIC RESPONSE OF RAMJET ENGINES TO FUEL FLOW RATE MODULATIONYu, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1357 PROOSIS - A COLLABORATIVE VENTURE FOR GAS TURBINE PERFORMANCE SIMULATION USING AN OBJECT ORIENTED PROGRAMMING SCHEMABala, A. / Pilidis, P. / Pachidis, V. / Gatto, E.L. / Sethi, V. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1358 NUMERICAL INVESTIGATION OF THE BLOWING CIRCUMFERENTIAL GROOVED CASING TREATMENTZhang, H.-G. / Chu, W. / Wu, Y. / Deng, W. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1359 SIMULATION-BASED PERFORMANCE ANALYSIS OF AXISYMMETRIC CASING TREATMENTS IN AXIAL COMPRESORSLepot, I. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1361 REAL TIME MONITORING OF DENSIFICATION DURING COLD AND WARM ISOSTATIC PRESSINGStevenson, J.F. / Zahrah, T.F. / Rowland, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1362 TRANSIENT MODELLING OF GEARTRAINS IN TWO-SHAFT AEROENGINESPeitsch, D. / Hanne, R. / Hartmann, T. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1363 CHARACTERISATION OF A REFURBISHED 1_STAGE TURBINE TEST RIG FOR FLOWFIELD MAPPING BEHIND BLADING WITH NON-AXISYMMETRIC CONTOURED ENDWALLSSnedden, G. / Roos, T. / Dunn, D. / Gregory-Smith, D. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1366 CONSTRUCTION OF A SUBSONIC TEST TURBINE FACILITY FOR EXPERIMENTAL INVESTIGATIONS OF SOUND GENERATION AND PROPAGATION FOR LOW PRESSURE TURBINESMoser, M. / Kulhanek, G. / Heitmeir, F. / Kahl, G. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1368 NUMERICAL INVESTIGATION OF THE TWO DIFFERENT CASING TREATMENTS IN A LOW SPEED CENTRIFUGAL COMPRESSORGao, P. / Li, W. / Yan, C. / Wu, H. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1369 NUMERICAL INVESTIGATION ON OFF-DESIGN PERFORMANCE OF A RADIAL INFLOW TURBINE FOR HYDROGEN-OXYGEN ROCKET ENGINESFeng, Z.-P. / Deng, Q.-H. / Niu, J. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1370 IMPROVING OF A VANED DIFFUSER FOR A GIVEN CENTRIFUGAL IMPELLER BASED ON CFD AND OPTIMIZATION METHODXi, G. / Wang, Z. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1371 MULTIDISCIPLINARY OPTIMIZATION OF THE CENTRIFUGAL IMPELLER OF A MICRO-GAS-TURBINE SYSTEMXi, G. / Wang, H. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1372 PROPULSION SYSTEM CONCEPTS FOR THE PLANETARY SURVEY MISSIONSFutamura, H. / Okai, K. / Yanagi, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1373 BAYESIAN PROBABILITY AND PROBABILITY DENSITY ESTIMATION: A HYBRID TECHNIQUE FOR PERFORMANCE DIAGNOSTICS IN GAS TURBINE ENGINESBechini, G. / Singh, R. / Probert, R. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1374 A SMALL-SCALE GAS TURBINE PERFORMANCE IMPROVEMENT APPROACHLi, Y.G. / American Institute of Aeronautics and Astronautics et al. | 2007
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AIAA-2007-1375 PARAMETRIC STUDY OF THE EVOLUTION OF A THIN LIQUID FILM STREAMING ON A HOLT TILTED PLATEHeid, G. / Giroud-Garapon, S. / American Institute of Aeronautics and Astronautics et al. | 2007