AIAA-2006-6150 Study on Flapping-of-Wings Flight of Butterfly with Numerical and Experimental Analysis (Englisch)
- Neue Suche nach: Senda, K.
- Neue Suche nach: Sawamoto, M.
- Neue Suche nach: Shibahara, T.
- Neue Suche nach: Kitamura, M.
- Neue Suche nach: Tanaka, T.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Neue Suche nach: Senda, K.
- Neue Suche nach: Sawamoto, M.
- Neue Suche nach: Shibahara, T.
- Neue Suche nach: Kitamura, M.
- Neue Suche nach: Tanaka, T.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
In:
AIAA atmospheric flight mechanics conference
;
452-467
;
2006
-
ISBN:
- Aufsatz (Konferenz) / Print
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Titel:AIAA-2006-6150 Study on Flapping-of-Wings Flight of Butterfly with Numerical and Experimental Analysis
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Beteiligte:Senda, K. ( Autor:in ) / Sawamoto, M. ( Autor:in ) / Shibahara, T. ( Autor:in ) / Kitamura, M. ( Autor:in ) / Tanaka, T. ( Autor:in ) / American Institute of Aeronautics and Astronautics
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Kongress:AIAA atmospheric flight mechanics conference ; 2006 ; Keystone, Colo
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Erschienen in:AIAA ATMOSPHERIC FLIGHT MECHANICS CONFERENCE ; 1 ; 452-467
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Verlag:
- Neue Suche nach: American Institute of Aeronautics and Astronautics,
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Erscheinungsort:Reston:
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Erscheinungsdatum:01.01.2006
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Format / Umfang:16 pages
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Anmerkungen:Paper numbers 2006-6000 to 2006-6834 with gaps held
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ISBN:
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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.
- 1
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AIAA-2006-6000 T-50/A-50 Stores Separation ProgramKim, J. / Lee, I. / American Institute of Aeronautics and Astronautics et al. | 2006
- 14
-
AIAA-2006-6001 Pitch-Rate Induced Abrupt Wing Stalling of Straight Wing AircraftBeyers, M. / Brown, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 26
-
AIAA-2006-6002 Observations of Wake Vortex Instability Flowfields and Aircraft Response to EncountersBrown, A. / Bastian, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 40
-
AIAA-2006-6003 Data Reduction Issues for Performance Evaluation and Comparison of Flight Control LawsPerhinschi, M. / Napolitano, M. / Gururajan, S. / Seanor, B. / Burken, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 52
-
AIAA-2006-6004 Development of Light Aircraft Flight Test EquipmentIscold, P. / Mol, F. / Brasil, N. S. / Maciel, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 65
-
AIAA-2006-6005 POD as a Surrogate Modeling Technique in Parametric Studies of Weapon AerodynamicsMifsud, M. / Shaw, S. / Bennett, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 80
-
AIAA-2006-6006 Time-Accurate Computations of Free-Flight Aerodynamics of a Spinning Projectile with Flow ControlSahu, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 90
-
AIAA-2006-6007 On Implementation of Trajectory Correction System on a Routinely Used Artillery RocketGhosh, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 103
-
AIAA-2006-6008 Another Analytical Approach to Predicting Direct-Fire Munition TrajectoriesCooper, G. / Weinacht, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 116
-
AIAA-2006-6009 Experimental Determination of the Effect of Rifling Grooves on the Aerodynamics of Small Caliber ProjectilesSilton, S. / Webb, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 128
-
AIAA-2006-6010 Validation and Prediction of the Effect of Rifling Grooves on Small-Caliber Ammunition PerformanceWeinacht, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 140
-
AIAA-2006-6130 Modeling and Simulation of 9-DOF Parafoil-Payload System Flight DynamicsPrakash, O. / Ananthkrishnan, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 166
-
AIAA-2006-6131 Determination of Dynamic Stability Information Through Simulation of a Tumbling Tailless AircraftSaephan, S. / van Dam, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 181
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AIAA-2006-6132 Cable-Supported Sliding Payload Deployment from a Fixed-Wing AircraftWilliams, P. / Trivailo, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 203
-
AIAA-2006-6134 Analysis of Different Stabilizing Control Systems for Aircraft with Automated Cruise FlapsCox, C. / Gopalarathnam, A. / Hall, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 214
-
AIAA-2006-6135 Flight Dynamics of High Aspect-Ratio Flying WingsRaghavan, B. / Patil, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 226
-
AIAA-2006-6136 Performance Assessment Based on Nonlinear Constraints Imposed on Complex Simulation ModelsHolzapfel, F. / Lenz, J. / Sachs, G. / Leitner, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 250
-
AIAA-2006-6137 Computations of Viking Lander Capsule Hypersonic Aerodynamics with Comparisons to Ground and Flight DataEdquist, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 270
-
AIAA-2006-6138 Ablation Modeling for Dynamic Simulation of Reentry VehiclesDoman, D. / Blake, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 288
-
AIAA-2006-6140 Parametric Shape Study of Capsule-Type Vehicles During Atmospheric Re-EntryShweyk, K. / Tamrat, B. / Khodadoust, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 302
-
AIAA-2006-6141 Robust/Optimal Temperature Profile Control of a Re-Entry Vehicle Using Neural NetworksYadav, V. / Padhi, R. / Balakrishnan, S. / American Institute of Aeronautics and Astronautics et al. | 2006
- 335
-
AIAA-2006-6142 Metamodeling and Optimisation Applied to the Selection of the Configuration of Atmospheric Entry VehiclesRamos, R. H. / Bonetti, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 345
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AIAA-2006-6144 Practical Aspects of the Equation-Error Method for Aircraft Parameter EstimationMorelli, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 363
-
AIAA-2006-6145 Global Modeling of Pitch Damping from Flight DataFavaregh, N. / Landman, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 376
-
AIAA-2006-6146 Aerodynamic Parameter Estimation from Flight Data Applying Extended and Unscented Kalman FilterChowdhary, G. / Jategaonkar, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 394
-
AIAA-2006-6147 System Identification of the Longitudinal/Heave Dynamics for a Tandem-Rotor Helicopter Including Higher-Order DynamicsLawler, M. / Ivler, C. / Tischler, M. / Shtessel, Y. / American Institute of Aeronautics and Astronautics et al. | 2006
- 426
-
AIAA-2006-6148 Oscillation Amplitude Growth for a Decelerating Object with Constant Pitch DampingSchoenenberger, M. / Queen, E. / Litton, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 440
-
AIAA-2006-6149 Estimation of Drag Coefficient from Flight Data of a Cargo ShellDutta, G. / Ghosh, A. / Singhal, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 452
-
AIAA-2006-6150 Study on Flapping-of-Wings Flight of Butterfly with Numerical and Experimental AnalysisSenda, K. / Sawamoto, M. / Shibahara, T. / Kitamura, M. / Tanaka, T. / American Institute of Aeronautics and Astronautics et al. | 2006
- 468
-
AIAA-2006-6152 Coning Motion of Nozzle-First Cone Cylinder Body at High Angles of AttackYoshinaga, T. / Nakayama, K. / Tate, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 481
-
AIAA-2006-6153 T-50/A-50 High Angle of Attack CharacteristicsLee, M. / Lee, Y. / Lee, I. / American Institute of Aeronautics and Astronautics et al. | 2006
- 495
-
AIAA-2006-6154 Estimation of Longitudinal Unsteady Aerodynamics of a Wing-Tail Combination from Wind Tunnel DataMurphy, P. / Klein, V. / American Institute of Aeronautics and Astronautics et al. | 2006
- 508
-
AIAA-2006-6267 Analytical Criterion for Onset of Departure in Inertia-Coupled Roll Maneuvers of AirplanesMahale, A. / Ananthkrishnan, N. / American Institute of Aeronautics and Astronautics et al. | 2006
- 527
-
AIAA-2006-6268 Trailing Vortex Wake Encounters at Altitude - A Potential Flight Safety Issue?Nelson, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 544
-
AIAA-2006-6270 Survey of Jet Transport Incident/Accidents with Pitch Rate Induced Abrupt Wing Stalling Near the GroundBrown, A. / Beyers, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 558
-
AIAA-2006-6271 A Performance-Based Method for Improving Safety During Runway ManeuversZammit-Mangion, D. / Zammit, B. / Sammut, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 569
-
AIAA-2006-6272 A Traffic Movement Monitoring Computer for Pre-Emptive Runway Conflict DetectionSammut, A. / Zammit, B. / Zammit-Mangion, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 580
-
AIAA-2006-6273 Aerothermodynamic Optimization of Re-Entry Heat Shield Shapes for a Crew Exploration VehicleJohnson, J. / Starkey, R. / Lewis, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 595
-
AIAA-2006-6274 Multidimensional Aerothermodynamic Analysis for Planetary Probes Using OLAP CubesSubrahmanyam, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 622
-
AIAA-2006-6275 Reentry Envelope Determination Part II: Structural Failure due to Heating and UncertaintiesReynerson, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 644
-
AIAA-2006-6276 An Evaluation of Ballute Entry Systems for Lunar Return MissionsClark, I. / Wells, G. / Theisinger, J. / Braun, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 659
-
AIAA-2006-6279 Attitude Estimation Using an Accelerometer Based DeviceCrassidis, A. / Chheda, B. / Long, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 670
-
AIAA-2006-6280 Optimal Experiment and Input Design for Flight Test Protocol OptimizationSeren, C. / Bommier, F. / Verdier, L. / Bucharles, A. / Alazard, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 682
-
AIAA-2006-6281 A Neural Model of Coefficients of Forces and Moments of Aerodynamic Forces for a Turboprop AircraftManerowski, J. / Sibilski, K. / Zgrzywa, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 692
-
AIAA-2006-6282 Air Data System Calibration of T-50/A-50Roh, H. / Park, Y. / Park, N. / Lee, I. / American Institute of Aeronautics and Astronautics et al. | 2006
- 702
-
AIAA-2006-6283 Aircraft Parameter Estimation Experiment Design Considering Measurement Colored ResidualsNeto, N. S. B. / Goes, L. / Hemerly, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 714
-
AIAA-2006-6284 Parameter Estimation from Flight Data of a Missile Using Maximum Likelihood and Neural Network MethodSingh, S. / Ghosh, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 735
-
AIAA-2006-6370 The Bifurcation Tailoring of Nonlinear Entomopter ControlSibilski, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 761
-
AIAA-2006-6371 Alternative Derivation of the Euler Axis Kinematic Differential Equation Using Eigensystem DerivativesBurchett, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 771
-
AIAA-2006-6372 A Dynamic Performance Evaluation Technique for Unmanned Aerial VehiclesSadraey, M. / Colgren, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 789
-
AIAA-2006-6374 Periodic Solutions for Flexible Cable-Body Systems Towed in Circular and Elliptical PathsWilliams, P. / Trivailo, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 811
-
AIAA-2006-6375 Dynamics and Equilibrium of a Twin-Aircraft-Cable System for Payload RetrievalWilliams, P. / Trivailo, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 832
-
AIAA-2006-6378 A Tool for Integrating Commercial Space Operations into the National Airspace SystemMurray, D. / VanSuetendael, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 838
-
AIAA-2006-6379 A Strategy for Reducing Hazards from Reentry DebrisAilor, W. / Bonaparte, L. / Shelton, F. / American Institute of Aeronautics and Astronautics et al. | 2006
- 845
-
AIAA-2006-6381 Guided Weapon Danger Area Generation - Implementing A Probabilistic ApproachFletcher, D. / Wilson, S. / Jokic, M. / Vuletich, I. / American Institute of Aeronautics and Astronautics et al. | 2006
- 855
-
AIAA-2006-6485 Significance of Unsteady Aerodynamic Effects in F/A-18C/D Pitching MomentHeller, M. / Holmberg, J. / David, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 866
-
AIAA-2006-6486 High-Alpha Trim and Stability Analysis of Aircraft Closed-Loop Dynamics with Control SaturationAnanthkrishnan, N. / Ghosh, K. / Paranjape, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 895
-
AIAA-2006-6489 Estimation of Nonlinear Aerodynamic Models for Identification of Uncommanded Rolling MotionsLan, C. / Bianchi, S. / Brandon, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 920
-
AIAA-2006-6490 Effects of Bearing Friction of Rolling Test Rig on Transonic Roll DampingLan, C. / Bianchi, S. / Brandon, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 938
-
AIAA-2006-6492 Determination of Maximum Unnoticeable Added DynamicsMitchell, D. / Hoh, R. / He, C. / Strope, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 954
-
AIAA-2006-6493 The Use of Flight Simulation for Research and Teaching in AcademiaWhite, M. / Padfield, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 968
-
AIAA-2006-6494 Effects of Aeroelasticity on the Pilots Psychomotor BehaviorGroot, T. / Damveld, H. / Mulder, M. / Van Paassen, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 992
-
AIAA-2006-6495 Identifying a PIO Signature - New Techniques Applied to an Old ProblemMitchell, D. / Klyde, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1007
-
AIAA-2006-6496 Flight Test Experience with Eurofighter Typhoon During High Bandwidth PIO Resistance TestingOelker, H. / Brieger, O. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1019
-
AIAA-2006-6497 Analysis of Requirements for Directional DynamicsLee, B. / Rodchenko, V. / Zaichik, L. / Perebatov, V. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1029
-
AIAA-2006-6498 Analysis of Pilot Landing Control Using Neural NetworkSakamoto, Y. / Mori, R. / Suzuki, S. / Takahara, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1036
-
AIAA-2006-6499 A Tiered Approach to Flight Safety AnalysisMurray, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1047
-
AIAA-2006-6500 Hazard Analysis for Uncontrolled Space Vehicle ReentryPatera, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1064
-
AIAA-2006-6501 Debris Field Estimation Methods for the STS-107 Columbia InvestigationGraybeal, S. / Mrozinski, R. / Mendeck, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1073
-
AIAA-2006-6502 RTI Horizons Overflight Risk Analysis Toolset Risk ProcessorDevoid, W. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1079
-
AIAA-2006-6503 Multi-Resolution Global Population Model for Overflight Risk AnalysesDevoid, W. / Laney, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1088
-
AIAA-2006-6504 Boom and Receptacle Autonomous Air Refueling Using a Visual Pressure Snake Optical SensorDoebbler, J. / Valasek, J. / Monda, M. / Schaub, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1111
-
AIAA-2006-6505 Flight Dynamics of a Morphing Aircraft Utilizing Independent Multiple-Joint Wing SweepGrant, D. / Abdulrahim, M. / Lind, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1126
-
AIAA-2006-6506 GPS Autopilot Without Rate Sensors for UAV AircraftMcCue, M. / Biezad, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1138
-
AIAA-2006-6507 In-Flight Reconfigurable Autopilot for Unmanned Aircraft: Hardware Development and Flight Test ResultsSarigul-Klijn, N. / Huber, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1159
-
AIAA-2006-6508 The Development of a Thin/Cambered/Reflexed Airfoil for Micro Air Vechhicle Applications at Reynolds Numbers of 60,000 to 100,000Reid, M. / Kozak, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1165
-
AIAA-2006-6510 Near-Space Station Keeping Performance of a Large High-Altitude Notional AirshipSchmidt, D. / Stevens, J. / Roney, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1174
-
AIAA-2006-6632 Prediction of VRS Using Ring Vortex Model for Single-Rotor and Multi-Rotor ConfigurationsPrasad, J. / Chen, C. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1183
-
AIAA-2006-6633 Prediction of Helicopter Critical Flight Regimen by Continuation and Bifurcation MethodsSibilski, K. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1210
-
AIAA-2006-6634 Flight Dynamics Analysis of Periodically Forced Rotorcraft ModelBedford, R. / Lowenberg, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1229
-
AIAA-2006-6636 Sonic Boom Mitigation Through Thickness, Camber and Nose Angle Optimizations for a Delta WingKandil, O. / Khasdeo, N. / Ozcer, I. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1241
-
AIAA-2006-6637 A Hypersonic Vehicle Model Developed Using Piston TheoryOppenheimer, M. / Doman, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1261
-
AIAA-2006-6638 Flight Mechanics and Control Issues for Micro Aerial VehiclesStewart, K. / Abate, G. / Evers, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1277
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AIAA-2006-6639 Aerodynamics and Controls Design for Autonomous Micro Air VehiclesShkarayev, S. / Krashanitsa, R. / Platanitis, G. / Silin, B. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1294
-
AIAA-2006-6640 Wind Tunnel Database Development and Nonlinear Modeling Applied to Powered Micro Aerial Vehicles with Flexible WingsAlbertani, R. / Ifju, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1308
-
AIAA-2006-6641 Minimum-Effort Guidance for Vision-Based Collision AvoidanceWatanabe, Y. / Calise, A. / Johnson, E. / Evers, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1317
-
AIAA-2006-6642 Navigation and Control Problems for Classes of Micro Air VehiclesHamilton, H. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1328
-
AIAA-2006-6643 Using Avian Morphology to Enhance Aircraft ManeuverabilityAbdulrahim, M. / Lind, R. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1345
-
AIAA-2006-6644 A Trajectory Determination Approach for MAVs Using Genetic AlgorithmsAnderson, M. / Lopez, J. / Evers, J. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1357
-
AIAA-2006-6645 The Descent from Altitude Problem (A Conventional Approach)Baker, A. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1370
-
AIAA-2006-6646 Modelling Unsteady Heating Effects on the Structural Dynamic of a Hypersonic VehicleBolender, M. / Doman, D. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1391
-
AIAA-2006-6647 Flexible Mode Analysis of a Hypersonic VehicleWilliams, T. / Bolender, M. / Doman, D. / Morataya, O. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1413
-
AIAA-2006-6648 Modeling and Control of a Recoverable Balloon System for Launch of Small Payloads to Low Earth OrbitCrassidis, A. / Wilson, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1426
-
AIAA-2006-6824 Atmospheric Flight Mechanics Education - Are the Customers Getting What They Need?Field, E. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1439
-
AIAA-2006-6826 Response of Graphite/Epoxy Structures to the Reentry EnvironmentAilor, W. / Baker, R. / Bonaparte, L. / Hallman, W. / Moody, D. / Steckel, G. / Weaver, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1449
-
AIAA-2006-6827 A Single Flight Path Tool For Use In Dynamic Range SafetyTorres, J. / Rohl, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1458
-
AIAA-2006-6828 Space Shuttle Public Entry Risk Assessment and MitigationMrozinski, R. / Mendeck, G. / Graybeal, S. / Schottel, M. / Chi, G. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1467
-
AIAA-2006-6832 The Development of a Thin/Cambered/Reflexed Airfoil for Micro Air Vehicle Applications at Reynolds Numbers of 60,000 to 100,000Reid, M. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1473
-
AIAA-2006-6833 Multidimensional Aerothermodynamic Analysis for Planetary Probes Using OLAP CubesSubrahmanyam, P. / American Institute of Aeronautics and Astronautics et al. | 2006
- 1500
-
AIAA-2006-6834 Prediction of Icing Effects on the Lateral/Directional Stability and Control of Light AirplanesLampton, A. / Valasek, J. / American Institute of Aeronautics and Astronautics et al. | 2006