Transonic Blunt Body Aerodynamic Coefficients Computation (Englisch)
- Neue Suche nach: Sancho, J.
- Neue Suche nach: Vargas, M.
- Neue Suche nach: Gonzalez, E.
- Neue Suche nach: Rodriguez, M.
- Neue Suche nach: European Space Agency
- Neue Suche nach: Sancho, J.
- Neue Suche nach: Vargas, M.
- Neue Suche nach: Gonzalez, E.
- Neue Suche nach: Rodriguez, M.
- Neue Suche nach: European Space Agency
In:
European Symposium on Aerothermodynamics
692
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148
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2011
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ISBN:
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ISSN:
- Aufsatz (Konferenz) / Print
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Titel:Transonic Blunt Body Aerodynamic Coefficients Computation
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Beteiligte:Sancho, J. ( Autor:in ) / Vargas, M. ( Autor:in ) / Gonzalez, E. ( Autor:in ) / Rodriguez, M. ( Autor:in ) / European Space Agency
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Kongress:7th, European Symposium on Aerothermodynamics ; 2011 ; Bruges, Belgium
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Erschienen in:European Symposium on Aerothermodynamics , 692 ; 148EUROPEAN SPACE AGENCE - PUBLICATIONS - ESA SP , 692 ; 148
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Verlag:
- Neue Suche nach: ESA Communications
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Erscheinungsort:Noordwijk
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Erscheinungsdatum:01.01.2011
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Format / Umfang:148 pages
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Anmerkungen:Held in e-store (RMS)
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ISBN:
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ISSN:
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Medientyp:Aufsatz (Konferenz)
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Format:Print
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Sprache:Englisch
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Schlagwörter:
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Datenquelle:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Inhaltsverzeichnis Konferenzband
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
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- 2
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ExoMars Entry Demonstrator Module AerodynamicsTran, P. / Beck, J. / European Space Agency et al. | 2011
- 3
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Measurements on the ExoMars Configuration in the High Enthalpy Shock Tunnel Gottingen (HEG)Martinez-Schramm, J. / Wagner, A. / Hannemann, K. / European Space Agency et al. | 2011
- 4
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Aerothermodynamics of the ExoMars Entry Demonstrator ModuleBeck, J. / Tran, P. / Walpot, L. / European Space Agency et al. | 2011
- 5
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ONERA Experimental Contribution to ExoMars ProjectViguier, P. / Verant, J.L. / Mohamed, A.K. / European Space Agency et al. | 2011
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- 7
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- 8
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Experimental Study of the Dynamic Stability of the ExoMars CapsuleGulhan, A. / Klevanski, J. / Willems, S. / European Space Agency et al. | 2011
- 9
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Radiative Heating of the ExoMars Entry Demonstrator ModuleBeck, J. / Omaly, P. / da Silva, M.L. / Surzhikov, S. / European Space Agency et al. | 2011
- 10
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Experimental Study of ExoMars Sub- and Transonic Aerodynamics and Heat Shield Separation in HSTNeeb, D. / Gulhan, A. / Augenstein, E. / European Space Agency et al. | 2011
- 11
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Windtunnel Rebuilding and Extrapolation to Flight at Transsonic Speed for ExoMarsFertig, M. / Neeb, D. / Gulhan, A. / European Space Agency et al. | 2011
- 12
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ExoMars Entry Demonstrator Module Dynamic StabilityDormieux, M. / Gulhan, A. / Berner, C. / European Space Agency et al. | 2011
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Preliminary Results of the Collisional-Radiative Model CoRaM-Mars: Focus on C, N, O and AR Ionization/Recombination and CO~2 Dissociation/RecombinationAnnaloro, J. / Bultel, A. / Omaly, P. / European Space Agency et al. | 2011
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- 17
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- 21
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Radiative Aerothermodynamics of Entry Probes in Martian and Earth AtmosphereSurzhikov, S.T. / Shang, J.S. / European Space Agency et al. | 2011
- 22
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Heat Transfer in Sub- and Supersonic Nonequilibrium Jets of Carbon Dioxide PlasmasKolesnikov, A.F. / Gordeev, A.N. / Vasilevskii, S.A. / European Space Agency et al. | 2011
- 23
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Equilibrium Radiation Measurements and Simulations for Earth and Martian Atmospheric EntryBrandis, A.M. / Cruden, B.A. / Prabhu, D. / European Space Agency et al. | 2011
- 24
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The SCRAMSPACE I Scramjet Flight Experiment - Scientific Rationale and Technical DevelopmentsTirtey, S.C. / Boyce, R.R. / Brown, L. / European Space Agency et al. | 2011
- 25
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Ground-Based Testing of the HyShot II Combustor Using OH^* ChemiluminiscenceLaurence, S.J. / Schramm, J.M. / Karl, S. / Hannemann, K. / European Space Agency et al. | 2011
- 26
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Starting Mechanisms for High Contraction Ratio Hypersonic InletsGrainger, A. / Tirtey, S.C. / Boyce, R.R. / European Space Agency et al. | 2011
- 27
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Experimental and Numerical Investigations on Mixing and Combustion Processes in a Supersonic Model CombustorFuhrmann, S. / Paukner, D. / Hupfer, A. / Kau, H.-P. / European Space Agency et al. | 2011
- 28
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Design of a Scramjet Nozzle with Streamline Tracing Technique and Reference Temperature MethodRiehmer, J. / Gulhan, A. / European Space Agency et al. | 2011
- 29
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Supercritical Fluid Injection: An Experimental StudyLamanna, G. / Stotz, I. / Weigand, B. / Steelant, J. / European Space Agency et al. | 2011
- 30
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Overview of Suborbital Human Transportation Concept ALPHAAdirim, H. / Pilz, N. / Marini, M. / European Space Agency et al. | 2011
- 31
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System Analyses Driving Improved Aerothermodynamic Lay-Out of the SpaceLiner ConfigurationSippel, M. / van Foreest, A. / Dietlein, I. / European Space Agency et al. | 2011
- 32
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Direct Numerical Simulation of Mixing Enhancement in Supersonic Shear FlowsLee, I.L. / Sandham, N.D. / European Space Agency et al. | 2011
- 33
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Numerical Simulation of Shock Response to Wall Changes in High Speed IntakesFincham, J. / Taylor, N.V. / European Space Agency et al. | 2011
- 34
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Nozzle Numerical Analysis of the SCIMITAR EngineBattista, F. / Marini, M. / Cutrone, L. / European Space Agency et al. | 2011
- 35
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FAST20XX: Achievements on European Suborbital Space FlightMack, A. / Steelant, J. / Adirim, H. / European Space Agency et al. | 2011
- 36
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European Activities on High Speed Vehicles: Feasibility Studies and Technological Challenges for Hypersonic CruisersSteelant, J. / European Space Agency et al. | 2011
- 37
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Preliminary Design of the Low Speed Propulsion Air Intake of the LAPCAT-MR2 AircraftMeerts, C. / Steelant, J. / Hendrick, P. / European Space Agency et al. | 2011
- 38
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Waverider Design Using a Generalised Flare FlowfieldMurray, N. / European Space Agency et al. | 2011
- 39
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Experimental and Numerical Study of CMC Leading Edges in Hypersonic FlowsKuhn, M. / Esser, B. / Gulhan, A. / European Space Agency et al. | 2011
- 40
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Intermediate Experimental Vehicle, ESA Program IXV ATDB Tool and Aerothermodynamic CharacterizationMareschi, V. / Ferrarella, D. / Zaccagnino, E. / European Space Agency et al. | 2011
- 41
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Characterization of the IXV Thermal Protection System in High Enthalpy Plasma FlowPanerai, F. / Helber, B. / Sakraker, I. / European Space Agency et al. | 2011
- 42
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Intermediate eXperimental Vehicle, ESA program Supersonic-Transonic AerodynamicsSjors, K. / Olsson, J. / Maseland, H. / European Space Agency et al. | 2011
- 43
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Intermediate eXperimental Vehicle, ESA Program Aerothermodynamics - Transition and Steps and Gaps AssessmentVerant, J.-L. / Pelissier, C. / Sourgen, F. / European Space Agency et al. | 2011
- 44
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Design and Validation of a Temperature Measurement System for the Movable Flaps on the IXVWalz, S. / Roesgen, T. / Pereira, C. / European Space Agency et al. | 2011
- 45
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Flow-Field over Slender and Blunt Bodies in Hypersonic Non-Equilibrium FlowsBelouaggadia, N. / Takayam, K. / Brun, R. / Oliver, H. / European Space Agency et al. | 2011
- 46
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Experimental and Numerical Investigation of Aerothermal Characteristics of the IXV Hypersonic VehicleParis, S. / Charbonnier, D. / Tran, D. / European Space Agency et al. | 2011
- 47
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CFD Aerothermodynamic Characterization of the IXV Hypersonic VehicleRoncioni, P. / Ranuzzi, G. / Marini, M. / European Space Agency et al. | 2011
- 48
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Aerothermochemistry Testing for Lifting Reentry VehiclesChazot, O. / Panerai, F. / van der Haegen, V. / European Space Agency et al. | 2011
- 49
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Coupling Between the Mission Analysis and Flight Mechanics of IXV and the Aerothermodynamics Database ToolHaya-Ramos, R. / Serna, J. / Parigini, C. / European Space Agency et al. | 2011
- 50
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Determination by CFD of the IXV Aerodynamic Coefficients and RCS Yaw EfficiencyQuintino, T. / Xia, Y. / Banyai, T. / Rambaud, P. / European Space Agency et al. | 2011
- 51
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Direct Monte Carlo Simulations of the Intermediate eXperimental Vehicle at Early Stages of ReentryBanyai, T. / Torres, E. / Kashkovsky, A.V. / European Space Agency et al. | 2011
- 52
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ESA Intermediate Experimental Vehicle. Independent Aerothermodynamic Characterization and Aerodatabase DevelopmentRufolo, G.C. / Di Benedetto, S. / Walpot, L. / European Space Agency et al. | 2011
- 53
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Feasibility of Optical Measurement of Control Surface Movement During Re-EntryGruenberg, T. / Roesgen, T. / Walz, S. / Pereira, C. / European Space Agency et al. | 2011
- 54
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Instrumentation of C-SiC Tiles to Quantify their Mechanical Behaviour During Atmospheric Re-EntryPereira, C. / Romano, R. / Walz, S. / European Space Agency et al. | 2011
- 55
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Review of Non-Equilibrium Atmospheric Entry In-Flight InstrumentationsHerdrich, G. / Fertig, M. / Fasoulas, S. / European Space Agency et al. | 2011
- 56
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Design of a Scientific Experiment on EXPERT Flap at CIRA SCIROCCO Plasma Wind TunnelTrifoni, E. / Del Vecchio, A. / Di Clemente, M. / European Space Agency et al. | 2011
- 57
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Thermostructural Characterization of Materials of the EXPERT CapsuleDel Vecchio, A. / Gardi, R. / Reimer, T. / European Space Agency et al. | 2011
- 58
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Aerothermodynamics of EXPERT Control SurfacesGulhan, A. / Pereira, C. / Di Clemente, M. / European Space Agency et al. | 2011
- 59
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Expert Cold Structure DevelopmentAtkins, T. / Demuyere, P. / European Space Agency et al. | 2011
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Development of Metallic Thermal Protection System for the EXPERT Re-Entry Vehicle: Design VerificationFatemi, J. / European Space Agency et al. | 2011
- 61
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EXPERT - Demonstrating Reentry Aerothermodinamics Phenomena from a System PerspectiveMassobrio, F. / Passarelli, G. / Gavira-Izquierdo, J. / Ratti, F. / European Space Agency et al. | 2011
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Prediction of the Critical Distributed Roughness Height Inducing Transition on the EXPERT VehicleGrossir, G. / Paris, S. / Chazot, O. / Rambaud, P. / European Space Agency et al. | 2011
- 63
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Aero-Thermo Structural Simulation of the EXPERT Flaps in Plasma Wind Tunnel ConditionsMuller, T. / Tirtey, S.C. / Boyce, R.R. / European Space Agency et al. | 2011
- 64
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Aerothermal Assment of the EXPERT Flap in the SCIROCCO Wind TunnelWalpot, L. / Di Clemente, M. / Vos, J. / European Space Agency et al. | 2011
- 65
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Design and Ground Testing for the EXPERT PL4/PL5 `Natural and Roughness Induced Transition'Masutti, D. / Chazot, O. / Donelli, R. / de Rosa, D. / European Space Agency et al. | 2011
- 66
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A Prospective of Physical Modeling for Nonequilibrium Radiative Hypersonic Flow SimulationShang, J.S. / Surzhikov, S.T. / European Space Agency et al. | 2011
- 67
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Detailed Theoretical Study of Collisional Rotation-Vibration Energy Transfer and Dissociation in N~2Jaffe, R.L. / Schwenke, D.W. / Panesi, M. / Magin, T.E. / European Space Agency et al. | 2011
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Application of Vibrational State to State Collisional Models for Atmospheric Entry FlowsMunafo, A. / Panesi, M. / Jaffe, R. / European Space Agency et al. | 2011
- 69
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Influence of Internal Energy Excitation and Molecular Dissociation on Normal Shock StructureTorres, E. / Munafo, A. / Magin, T. / European Space Agency et al. | 2011
- 70
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Application of Quantum Mechanic and Quasi-Classical Models of Elementary Processes in High Temperature Gases for Computational Models of Entry Probes Aero PhysicsSurzhikov, S.T. / European Space Agency et al. | 2011
- 71
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Recent Advancements in the Numerical Simulation of Non-Equilibrium Flows with Application to Monatomic GasesKapper, M.G. / Cambier, J.-I. / Bultel, A. / Magin, T.E. / European Space Agency et al. | 2011
- 72
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The Chemical Elemental Demixing in the Simulation of Flows in the Inductive Plasmatron ChamberSakharov, V.I. / Khanukaeva, D.Y. / European Space Agency et al. | 2011
- 73
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Simplified Thermo-Chemical Modelling for Hypersonic FlowSancho, J. / Alvarez, P. / Gonzalez, E. / Rodiguez, M. / European Space Agency et al. | 2011
- 74
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Thermal and Chemical Non-Equilibrium Effects in the Wake of a Boundary-Layer Sized Object in Hypersonic FlowsBirrer, M. / Stemmer, C. / Adams, N.N. / European Space Agency et al. | 2011
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Heat Flux Measurement of Re-Entry Capsule Models under High-Enthalpy High-Pressure ConditionTanno, H. / Sato, K. / Komuro, T. / European Space Agency et al. | 2011
- 76
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On Numerical Methods for Hypersonic Turbulent FlowsYee, H.C. / Sjogreen, B. / Shu, C.W. / European Space Agency et al. | 2011
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Surface Pressure Measurements on a Flat Plate and a 7Deg Half-Cone at Mach 6Masutti, D. / Gunaydinoglu, E. / Chazot, O. / European Space Agency et al. | 2011
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Initial Experimental Verification of an Aerodynamic Heating Scaling Technique Applied to Supersonic Cone FlowsVeraar, R.G. / Bouquet, F. / European Space Agency et al. | 2011
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Stability Analyses and Validation of a Porous Surface Boundary Condition by Hypersonic Experiments on a Cone ModelWartemann, V. / Ludeke, H. / Willems, S. / Gulhan, A. / European Space Agency et al. | 2011
- 80
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Damping of the Second Mode Instability on a Cone in Hypersonic FlowWillems, S. / Gulhan, A. / European Space Agency et al. | 2011
- 81
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Investigation of Boundary Layer Transition in Three-Dimensional Supersonic Flow over Sharp ConeKozlovskiy, V.A. / Zemlyanskiy, B.A. / Kudryavtsev, V.V. / Shmanenkov, V.N. / European Space Agency et al. | 2011
- 82
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Feasibility Studies of Supersonic Laminar Flow Control Using a Grooved Wavy SurfaceNovikov, A.V. / Egorov, I.V. / European Space Agency et al. | 2011
- 83
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Linear Stability Analysis of Hypersonic Boundary LayerPinna, F. / Rambaud, P. / European Space Agency et al. | 2011
- 84
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Direct Numerical Simulation of Receptivity and Stability of a High-Speed Boundary LayerSoudakov, V.G. / Fedorov, A.V. / Ryzhov, A.A. / European Space Agency et al. | 2011
- 85
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Numerical Study of Compressible Mixing Layers with the DLR TAU CodeYou, Y. / Ludeke, H. / Hannemann, K. / European Space Agency et al. | 2011
- 86
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Design and Qualification of a Supersonic Wind Tunnel for Transition ExperimentsBottini, H. / Sonda, A. / Schreivogel, P. / Paniagua, G. / European Space Agency et al. | 2011
- 87
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Hypersonic Laminar-Turbulent Transition StudiesSaric, W. / Reed, H. / Bowersox, R. / North, S. / European Space Agency et al. | 2011
- 88
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Species and Temperature Gradient Measurements in the Reacting Boundary Layer over ICP Test SamplesFletcher, D.G. / Lutz, A.J. / Meyers, J.M. / European Space Agency et al. | 2011
- 89
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Highly Exothermic Surface Processes Relevant to the TPS Tiles: Oxygen Atom Adsorption on beta -Cristobalite and beta -QuartzRutigliano, M. / Cacciatore, M. / Zazza, C. / European Space Agency et al. | 2011
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A Short Review of Ablative-Material Response Models and Simulation ToolsLachaud, J. / Magin, T.E. / Cozmuta, I. / Mansour, N.N. / European Space Agency et al. | 2011
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SHARK: Flight Results of an UHTC-Based Nose Related to USV Hot StructuresGardi, R. / Del Vecchio, A. / Russo, G. / Marino, G. / European Space Agency et al. | 2011
- 92
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Unsteady Simulation of Hypersonic Flow over a Heat Probe in Ground Test ConditionsBensassi, K. / Lani, A. / Lico, A. / European Space Agency et al. | 2011
- 93
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Post Flight Analysis of SHEFEX I: Shock Tunnel Testing and Related CFD AnalysisMartinez-Schramm, J. / Barth, T. / Wagner, A. / Hannemann, K. / European Space Agency et al. | 2011
- 94
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Numerical Flight Mechanics Analysis of the SHEFEX I Ascent and Re-Entry PhasesCalvo, J.B. / Eggers, T. / European Space Agency et al. | 2011
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The SHEFEX II Thermal Protection SystemBohrk, H. / Elsasser, H. / Weihs, H. / European Space Agency et al. | 2011
- 96
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Experimental Study of SHEFEX II Hypersonic Aerodynamics and Canard Efficiency in H2KNeeb, D. / Gulhan, A. / European Space Agency et al. | 2011
- 97
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SHEFEX II Flight Instrumentation and Preparation of Post Flight AnalysisThiele, T. / Siebe, F. / Gulhan, A. / European Space Agency et al. | 2011
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Use of CFD for Fine Aerodynamic Characterisation of a LauncherPallegoix, J.-F. / Barrocca, B. / Brenner, P. / European Space Agency et al. | 2011
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Aeroelastic Analysis of Versatile Thermal Insulation Panels for Launcher ApplicationsCarrera, E. / Zappino, E. / Augello, G. / European Space Agency et al. | 2011
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Experimental and CFD Analysis of the Expansion Deflection NozzleTaylor, N.V. / European Space Agency et al. | 2011
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Launch Vehicle Base Buffeting - Recent Experimental and Numerical InvestigationsHannemann, K. / Ludeke, H. / Pallegoix, J.-F. / European Space Agency et al. | 2011
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Experimental Investigation of Base Flow Buffeting on the Ariane 5 Launcher Using High Speed PIVSchrijer, F.F.J. / Sciacchitano, A. / Scarano, F. / European Space Agency et al. | 2011
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On the Aerodynamic Heating of Vega Launcher: Compressible Chimera Navier-Stokes Simulation with Complex SurfacesDi Mascio, A. / Zaghi, S. / Muscari, R. / European Space Agency et al. | 2011
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Ground to Flight Extrapolation of SRM Radiative LoadsFerrara, V. / Paglia, F. / Mogavero, A. / European Space Agency et al. | 2011
- 105
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1St Stage Separation Aerodynamics of Vega LauncherGenito, M. / Paglia, F. / Mogavero, A. / Barbagallo, D. / European Space Agency et al. | 2011
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A Simplified Coupled Structural-Flowfield Analysis of Solid Rocket Motors Ignition TransientCavallini, E. / Favini, B. / Serraglia, F. / European Space Agency et al. | 2011
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A Fundamental Study of Free Shock Separation Induced Side-Loads within Conventional NozzlesAghababaie, A. / Taylor, N.V. / European Space Agency et al. | 2011
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Feasibility Analysis and Preliminary Design of an Atmospheric Re-Entry CubeSat DemonstratorBailet, G. / Asma, C.O. / Muylaert, J. / Magin, T. / European Space Agency et al. | 2011
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End to End Mission Analysis of the In Flight Research on Radiation Experiment (RADFLIGHT)Parigini, C. / Ramos, R.H. / Estepa, J.C.B. / European Space Agency et al. | 2011
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Coupled CFD-DSMC Simulations for Contamination Evaluation on Envisat Due to OCM Thruster PlumesPassaro, A. / Murray, N. / Snel, R. / Krieg, E. / European Space Agency et al. | 2011
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Spectroscopic Analysis of the Hayabusa Re-Entry Using Airborne and Ground Based EquipmentLohle, S. / Marynowski, T. / Mezger, A. / European Space Agency et al. | 2011
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CFD Studies of Supersonic Aerodynamics of the Earth Descent Module for Phobos-Grunt Interplanetary MissionEgorov, I.V. / Ivanov, D.V. / Nivikov, A.V. / European Space Agency et al. | 2011
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Uncertainty Quantification and Non-Deterministic Methodologies for CFD Based Design -The NODESIM-CFD ProjectHirsch, C. / Dinescu, C. / European Space Agency et al. | 2011
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Application of the DSMC Method to High-Temperature Nonequilibrium Flows with Chemical ReactionsBondar, Y.A. / Shevyrin, A.A. / Kashkovsky, A.V. / Ivanov, M.S. / European Space Agency et al. | 2011
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An Effective Treatment of Numerical Shock Wave Instabilities with Residual Distribution Schemes: Application to Hypersonic Flows around Blunt BodiesMena, J.G. / Lani, A. / Sermeus, K. / Deconinck, H. / European Space Agency et al. | 2011
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Molecular Simulation of Nonequilibrium Hypersonic FlowsSchwartzentruber, T.E. / Valentini, P. / Tump, P. / European Space Agency et al. | 2011
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Strong Coupling Algorithm to Solve Fluid-Structure-Interaction Problems with a Staggered ApproachVaassen, J.M. / De Vincenzo, P. / Hirsch, C. / Leonard, B. / European Space Agency et al. | 2011
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The Advanced Re-Entry Vehicle (ARV) a Development Step from ATV Toward Manned Transportation SystemsBottacini, M. / Berthe, P. / Vo, X. / Pietsch, K. / European Space Agency et al. | 2011
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Re-Entry Mission Analysis of the Advanced Re-entry Vehicle (ARV)Bonetti, D. / Haya-Ramos, R. / Strauch, H. / Bottacini, M. / European Space Agency et al. | 2011
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TPS Architecture on ARVSalmon, T. / Vo, X. / Bottacini, M. / European Space Agency et al. | 2011
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ARV Reentry Module Aerodynamics and AerothermodynamicsScheer, H. / Tran, P. / Berthe, P. / European Space Agency et al. | 2011
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Analysis of the ATV1 Re-Entry Using Near-UV Spectroscopic Data from the ESA/NASA Multi-Instrument Aircraft Observation CampaignLohle, S. / Marynowski, T. / Knapp, A. / European Space Agency et al. | 2011
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Forced Ignition Study Based on Wavelet MethodMartelli, E. / Valorani, M. / Paulucci, S. / Zikoski, Z. / European Space Agency et al. | 2011
- 124
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Laser Correlation Velocimetry Applied to a Flashing JetKamoun, H. / Lamanna, G. / Weigand, B. / Steelant, J. / European Space Agency et al. | 2011
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CFD Analysis of Radiative Heat Transfer in the SSME Main Combustion Chamber Using Advanced Spectral ModelsGobel, F. / Mundt, C. / European Space Agency et al. | 2011
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Large Eddy Simulation of Oxygen/Hydrogen Mixing Layers under Supercritical ConditionsNiedermeier, C.A. / Hickel, S. / Adams, N.A. / European Space Agency et al. | 2011
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Large Eddy Simulation of the Fuel Injection in Scramjet Combustion ChambersRana, Z.A. / Thornber, B.J.R. / Drikakis, D. / European Space Agency et al. | 2011
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Experimental and Numerical Modelling of the Priming Operation in Spacecraft Propulsion SystemsLema, M. / Pinho, J. / Steelant, J. / European Space Agency et al. | 2011
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SENARIET, a Programme to Solve Transient Flows of Liquids in Complex CircuitsVargas-Munoz, M. / Rodriguez-Fernandez, M. / Parena-Tapiador, A. / European Space Agency et al. | 2011
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Astrium Approach for Plume Flow and Impingement of 10 N Bipropellant ThrusterTheroude, C. / Scremin, G. / Wartelski, M. / European Space Agency et al. | 2011
- 131
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Implicit Large-Eddy Simulation of Heat Transfer in a Cooling Channel Using Supercritical Para-HydrogenChen, Z. / Hickel, S. / Adams, N.A. / European Space Agency et al. | 2011
- 132
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Numerical and Experimental Investigation on the Interface Shape of Cryogenic Fluids in Microgravity and Spinning ConditionsThibaut, A. / Cheuret, F. / Marraffa, L. / European Space Agency et al. | 2011
- 133
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A Density-Based Flow Solver for the Simulation of Sloshing in TanksMezine, M. / Dinescu, C. / Leonard, B. / Hirsch, C. / European Space Agency et al. | 2011
- 134
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Experimental-Analitical Procedure of Definition of Thermal Fluxes on the Head Fairing of Launch VechiclesYurchenko, I. / Karakotin, I. / Kudinov, A. / European Space Agency et al. | 2011
- 135
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Large Eddy and Reynolds-Averaged Navier-Stokes Simulations of an Underexpanded Sonic JetGorle, C. / Iaccarino, G. / European Space Agency et al. | 2011
- 136
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Peak Heat Fluxe Reduction Using Aerospikes Installed on Multimodule Launch VehicleKudinov, A. / Yurchenko, I. / Karakotin, I. / European Space Agency et al. | 2011
- 137
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Unsteady Phenomena in Transonic Flow over a Body of Revolution ShoulderKudryavtsev, V.V. / European Space Agency et al. | 2011
- 138
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Uncertainty Quantification for Gas-Surface Interaction in Plasmatron FacilityVilledieu, N. / Panerai, P. / Chazot, O. / Magin, T.E. / European Space Agency et al. | 2011
- 139
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Investigations of Surface-Catalyzed Reactions in a Mars MixtureDougherty, M. / Owens, W. / Meyers, J. / Fletcher, D.G. / European Space Agency et al. | 2011
- 140
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A Gas-Surface Interaction Model for the Numerical Study of High Temperature Flows over Pyrolyzing Ablative MaterialsTurchi, A. / Bianchi, D. / Nasuti, F. / European Space Agency et al. | 2011
- 141
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Investigation of the Gas-Surface Interaction of Innovative Carbon Composite Ablators in the VKI PlasmatronHelber, B. / Babou, Y. / Panerai, F. / European Space Agency et al. | 2011
- 142
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Ground Testing for GSI Database: What do we Determine?Chazot, O. / Panerai, F. / Marotta, M. / European Space Agency et al. | 2011
- 143
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A Finite-Rate-Catalytic Model for Hypersonic Flows Informed by Molecular DynamicsSchwartzentruber, T.E. / Valentini, P. / Norman, P. / Sorensen, C. / European Space Agency et al. | 2011
- 144
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MHD Experiment at CIRA GHIBLI Plasma Wind TunnelTrifoni, E. / Purpura, C. / Martucci, A. / European Space Agency et al. | 2011
- 145
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Investigations of a New Microwave Plasma Source Operating with Air, N~2, CO~2 and Argon GasesLe Quang, D. / Babou, Y. / Andre, P. / European Space Agency et al. | 2011
- 146
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Trajectory Analysis of the Reentry Vehicle with the Electromagnetic Flow ControlOtsu, H. / Katsurayama, H. / Konigorski, D. / Abe, T. / European Space Agency et al. | 2011
- 147
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Large Eddy Simulations of the 3D Subsonic Incompressible and Turbulent Flow over a Fixed Re-Entry Capsule at RE = 10 000Rasquin, M. / Degrez, G. / European Space Agency et al. | 2011
- 148
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Transonic Blunt Body Aerodynamic Coefficients ComputationSancho, J. / Vargas, M. / Gonzalez, E. / Rodriguez, M. / European Space Agency et al. | 2011
- 149
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Numerical Simulations of High-Altitude Aerothermodynamics of a Prospective Spacecraft ModelVashchenkov, P.V. / Kaskovsky, A.V. / Krylov, A.N. / Ivanov, M.S. / European Space Agency et al. | 2011
- 150
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The Russian Scientific Research Institute of Parachute Design and Production (NII Parachutostroyeniya, NIIPC) - History, Research and Collaboration in Space ProjectsLyalin, V. / Ladygin, V. / Komarov, V. / European Space Agency et al. | 2011
- 151
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Aerothermodynamic Insight from the HIFiRE ProgramKimmel, R.L. / Adamczak, D. / Dolvin, D. / European Space Agency et al. | 2011
- 152
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Experimental Studies at Duplicated Flight Conditions to Examine the Aerothermal Characteristic of the HIFIRE-1 and HIFIRE-5 Flight Test ConfigurationsHolden, M.S. / Wadhams, T.P. / MacLean, M. / Mundy, E. / European Space Agency et al. | 2011
- 153
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DNS of Transitional Flows on Cones at Hypersonic ConditionsCandler, G.V. / Johnson, H.B. / Drayna, T.W. / European Space Agency et al. | 2011
- 154
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FinEx - Fin Experiment on HIFiRE 5Bohrk, H. / Lohle, S. / Fuchs, U. / European Space Agency et al. | 2011
- 155
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Thermocouple Positioning for the Application of the Non-Integer System Identification Approach to HIFiRE-5 FinsLohle, S. / Bohrk, H. / Fuchs, U. / European Space Agency et al. | 2011
- 156
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Measurements of Instability and Transition in Hypersonic Boundary LayersCasper, K.M. / Schneider, S.P. / Beresch, S.J. / European Space Agency et al. | 2011
- 157
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Achievements and Perspectives of the PRORA-USV ProgramRichiello, C. / Russo, G. / Vecchione, L. / European Space Agency et al. | 2011
- 158
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Flight Results of USV-1 Dropped Transonic Flight Testsde Matteis, P. / Marino, G. / Richiello, C. / European Space Agency et al. | 2011
- 159
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Preliminary Analysis of the USV_2 Hypersonic Flight TestGuidotti, G. / Pezzella, G. / Richiello, C. / European Space Agency et al. | 2011
- 160
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Assessment of the Aerodynamic and Aerothermodynamic Performance of the USV-3 High-Lift Re-Entry VehiclePezzella, G. / Richiello, C. / Russo, G. / European Space Agency et al. | 2011
- 161
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USV UHTC-Based and WLE Experimental Test in SCIROCCO and CFD RebuildingMarino, G. / De Filippis, F. / Di Clemente, M. / Russo, G. / European Space Agency et al. | 2011
- 162
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Development of a Combined Sensor System for Atmospheric Entry MissionsPreci, A. / Eswein, N. / Herdrich, G. / Fasoulas, S. / European Space Agency et al. | 2011
- 163
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Investigation of Spatial and Temporal Flow Homogeneity in Arc-Jet Plasmas Using Intrusive and Non-Intrusive DiagnosticsCipullo, A. / Savino, L. / Graps, E. / European Space Agency et al. | 2011
- 164
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Enhancements to Compensating Nozzle Test Facilities at the University of BristolTaylor, N.V. / Aghababaie, A.A. / European Space Agency et al. | 2011
- 165
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Single Pulse Broadband Nitrogen CARS Measurements the High Enthalpy, Hypersonic Flow Field of L3K at Temperatures up to 5800 KFisher, M. / Koch, U. / Esser, B. / European Space Agency et al. | 2011
- 166
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Force Measurement Using Non-Restrained Models in a Shock TunnelTanno, H. / Sato, K. / Komuro, T. / European Space Agency et al. | 2011