Reviewers for 1 October 1999-30 September 2000 (Englisch)
In:
JOURNAL OF AIRCRAFT
;
38
;
6
;
2001
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ISSN:
- Aufsatz (Zeitschrift) / Print
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Titel:Reviewers for 1 October 1999-30 September 2000
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Erschienen in:JOURNAL OF AIRCRAFT ; 38 ; 6
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Verlag:
- Neue Suche nach: AMERICAN INST OF AERONAUTICS AND ASTRONAUTICS
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Erscheinungsdatum:01.01.2001
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Format / Umfang:6 pages
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ISSN:
-
Medientyp:Aufsatz (Zeitschrift)
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Format:Print
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Sprache:Englisch
- Neue Suche nach: 629.13334
- Weitere Informationen zu Dewey Decimal Classification
-
Klassifikation:
DDC: 629.13334 -
Datenquelle:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Inhaltsverzeichnis – Band 38
Zeige alle Jahrgänge und Ausgaben
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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Aircraft Technology Investment: The Affordability ProblemThomas M. Weeks et al. | 2001
- 1
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EDITORIAL - Aircraft Technology Investment: The Affordability ProblemWeeks, T.M. et al. | 2001
- 6
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Reviewers for 1 October 199930 September 2000| 2001
- 6
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EDITORIAL - Reviewers for 1 October 1990-30 September 2000| 2001
- 7
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Editorial Policy Statement on Numerical Accuracy and Experimental Uncertainty| 2001
- 7
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EDITORIAL - Editorial Policy Statement on Numerical Accuracy and Experimental Uncertainty| 2001
- 8
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EDITORIAL - Ethical Standards for Publication of Aeronautics and Astronautics Research| 2001
- 8
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Ethical Standards for Publication of Aeronautics and Astronautics Research| 2001
- 9
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AIAA Manuscript Review Process| 2001
- 9
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EDITORIAL - AIAA Manuscript Review Process| 2001
- 10
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Tail Buffet of F/A-18 at High Incidence with Sideslip and Roll (Part 1)S. Tavoularis / S. Marineau-Mes / A. Woronko / B. H. K. Lee et al. | 2001
- 10
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FULL-LENGTH PAPERS - Tail Buffet of F-A-18 at High Incidence with Sideslip and Roll (Part 1)Tavoularis, S. et al. | 2001
- 17
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FULL-LENGTH PAPERS - Tail Buffet of F-A-18 at High Incidence with Sideslip and Roll (Part 2)Tavoularis, S. et al. | 2001
- 17
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Tail Buffet of F/A-18 at High Incidence with Sideslip and Roll (Part 2)S. Tavoularis / S. Marineau-Mes / B. H. K. Lee et al. | 2001
- 22
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Numerical Study of a Wing-Tip Vortex Using the Euler EquationsRobert E. Spall et al. | 2001
- 22
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FULL-LENGTH PAPERS - Numerical Study of a Wing-Tip Vortex Using the Euler EquationsSpall, R.E. et al. | 2001
- 28
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Theoretical/Experimental Analysis of a Novel Airbreathing Device for Flow ControlT. M. A. Maksoud / A. Al-Shihry / J. Ward et al. | 2001
- 28
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FULL-LENGTH PAPERS - Theoretical-Experimental Analysis of a Novel Airbreathing Device for Flow ControlMaksoud, T.M.A. et al. | 2001
- 36
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Wing Rock of Nonslender Delta WingsLars E. Ericsson et al. | 2001
- 36
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FULL-LENGTH PAPERS - Wing Rock of Nonslender Delta WingsEricsson, L.E. et al. | 2001
- 42
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FULL-LENGTH PAPERS - Flutter Margin Evaluation for Discrete-Time SystemsTorii, H. et al. | 2001
- 42
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Flutter Margin Evaluation for Discrete-Time SystemsHiroshi Torii / Yuji Matsuzaki et al. | 2001
- 48
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Exploring the Feasibility of Pulsed Jet Separation Control for Aircraft ConfigurationsJohn C. Magill / Keith R. McManus et al. | 2001
- 48
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FULL-LENGTH PAPERS - Exploring the Feasibility of Pulsed Jet Separation Control for Aircraft ConfigurationsMagill, J.C. et al. | 2001
- 52
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FULL-LENGTH PAPERS - Investigation of a Circulation Controlled Cylinder Using an Adaptive Wall Wind TunnelDionisio, F.A. et al. | 2001
- 57
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Low-Speed Natural-Laminar-Flow Airfoils: Case Study in Inverse Airfoil DesignAshok Gopalarathnam / Michael S. Selig et al. | 2001
- 57
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FULL-LENGTH PAPERS - Low-Speed Natural-Laminar-Flow Airfoils: Case Study in Inverse Airfoil DesignGopalarathnam, A. et al. | 2001
- 64
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Nonlinear Dynamic Simulation of a Tethered Aerostat: A Fidelity StudyS. P. Jones / L. D. Schroeder et al. | 2001
- 64
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FULL-LENGTH PAPERS - Nonlinear Dynamic Simulation of a Tethered Aerostat: A Fidelity StudyJones, S.P. et al. | 2001
- 69
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Concurrently Optimized Aeroelastic Couplings and Rotor Stiffness for Alleviation of Helicopter Aeromechanical InstabilityEric Hathaway / Farhan Gandhi et al. | 2001
- 69
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FULL-LENGTH PAPERS - Concurrently Optimized Aeroelastic Couplings and Rotor Stiffness for Alleviation of Helicopter Aeromechanical InstabilityHathaway, E. et al. | 2001
- 81
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Accelerating Computational Fluid Dynamics Based Aeroelastic Predictions Using System IdentificationTimothy J. Cowan / Andrew S. Arena / Kajal K. Gupta et al. | 2001
- 88
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FULL-LENGTH PAPERS - Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance AircraftPatil, M.J. et al. | 2001
- 88
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Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance AircraftMayuresh J. Patil / Dewey H. Hodges / Carlos E. S. Cesnik et al. | 2001
- 95
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Development of a Scale Model Composite Fuselage Concept for Improved CrashworthinessKaren E. Jackson / Edwin L. Fasanella / Sotiris Kellas et al. | 2001
- 95
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FULL-LENGTH PAPERS - Development of a Scale Model Composite Fuselage Concept for Improved CrashworthinessJackson, K.E. et al. | 2001
- 104
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Displacement and Strain Statistics of Thermally Buckled PlatesJon Lee et al. | 2001
- 104
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FULL-LENGTH PAPERS - Displacement and Strain Statistics of Thermally Buckled PlatesLee, J. et al. | 2001
- 111
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Coupled Rotor/Fuselage Vibration Analysis for Teetering Rotor and Test Data ComparisonHyeonsoo Yeo / Inderjit Chopra et al. | 2001
- 111
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FULL-LENGTH PAPERS - Coupled Rotor-Fuselage Vibration Analysis for Teetering Rotor and Test Data ComparisonYeo, H. et al. | 2001
- 122
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Evaluating the Compressive Response of Notched Composite Panels Using Full-Field DisplacementsDavid M. McGowan / Damodar R. Ambur / T. Glen Hanna / Stephen R. McNeill et al. | 2001
- 130
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FULL-LENGTH PAPERS - Overview of Landing Gear DynamicsPritchard, J. et al. | 2001
- 130
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Overview of Landing Gear DynamicsJocelyn Pritchard et al. | 2001
- 138
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Probabilistic Fault Identification Using a Committee of Neural Networks and Vibration DataTshilidzi Marwala et al. | 2001
- 138
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FULL-LENGTH PAPERS - Probabilistic Fault Identification Using a Committee of Neural Networks and Vibration DataMarwala, T. et al. | 2001
- 147
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Time-Domain Reconstruction of Dynamic Multiaxial Responses in Aeronautical Fatigue TestingJan Eksteen / Anton Raath et al. | 2001
- 147
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FULL-LENGTH PAPERS - Time-Domain Reconstruction of Dynamic Multiaxial Responses in Aeronautical Fatigue TestingEksteen, J. et al. | 2001
- 154
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FULL-LENGTH PAPERS - Structural Wing Sizing for Multidisciplinary Design Optimization of a Strut-Braced WingGern, F.H. et al. | 2001
- 154
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Structural Wing Sizing for Multidisciplinary Design Optimization of a Strut-Braced WingFrank H. Gern / Amir H. Naghshineh-Pour / Erwin Sulaeman / Rakesh K. Kapania / Raphael T. Haftka et al. | 2001
- 164
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Feedforward Piezoelectric Structural Control: An Application to Aircraft Cabin Noise ReductionA. Grewal / D. G. Zimcik / B. Leigh et al. | 2001
- 164
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FULL-LENGTH PAPERS - Structural Loading of Outbound-Horizontal Stabilizer Aircraft Relative to Comparable Conventional DesignsKentfield, J.A.C. et al. | 2001
- 164
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FULL-LENGTH PAPERS - Feedforward Piezoelectric Structural Control: An Application to Aircraft Cabin Noise ReductionGrewal, A. et al. | 2001
- 174
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Structural Loading of Outbound-Horizontal Stabilizer Aircraft Relative to Comparable Conventional DesignsJ. A. C. Kentfield et al. | 2001
- 181
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Risk Analysis of Fuselage Splices Containing Multisite Damage and CorrosionM. Liao / Y. Xiong et al. | 2001
- 181
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FULL-LENGTH PAPERS - Risk Analysis of Fuselage Splices Containing Multisite Damage and CorrosionLiao, M. et al. | 2001
- 188
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ENGINEERING NOTES - Dynamic Stall Control by Intermittent Periodic ExcitationGreenblatt, D. et al. | 2001
- 188
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Dynamic Stall Control by Intermittent Periodic ExcitationD. Greenblatt / D. Neuburger / I. Wygnanski et al. | 2001
- 190
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Use of Periodic Excitation to Enhance Airfoil Performance at Low Reynolds NumbersDavid Greenblatt / Israel J. Wygnanski et al. | 2001
- 190
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ENGINEERING NOTES - Use of Periodic Excitation to Enhance Airfoil Performance at Low Reynolds NumbersGreenblatt, D. et al. | 2001
- 193
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FULL-LENGTH PAPERS - Vortical Flowfield Structure at Forward Swept-Wing ConfigurationsBreitsamter, C. et al. | 2001
- 193
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Vortical Flowfield Structure at Forward Swept-Wing ConfigurationsChristian Breitsamter / Boris Laschka et al. | 2001
- 208
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Flight Power Scaling of Airplanes, Airships, and Helicopters: Application to Planetary ExplorationRalph D. Lorenz et al. | 2001
- 208
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FULL-LENGTH PAPERS - Flight Power Scaling of Airplanes, Airships, and Helicopters: Application to Planetary ExplorationLorenz, R.D. et al. | 2001
- 215
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Multiagent Design Architecture for Intelligent Synthesis EnvironmentA. Deshmukh / T. Middelkoop / A. Krothapalli / W. Shields / N. Chandra / C. A. Smith et al. | 2001
- 215
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FULL-LENGTH PAPERS - Multiagent Design Architecture for Intelligent Synthesis EnvironmentDeshmukh, A. et al. | 2001
- 224
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FULL-LENGTH PAPERS - Using Artificial Neural Networks and Self-Organizing Maps for Detection of Airframe IcingJohnson, M.D. et al. | 2001
- 224
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Using Artificial Neural Networks and Self-Organizing Maps for Detection of Airframe IcingMatthew D. Johnson / Kamran Rokhsaz et al. | 2001
- 231
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Response Surface Method for Airfoil Design in Transonic FlowJaekwon Ahn / Hyoung-Jin Kim / Dong-Ho Lee / Oh-Hyun Rho et al. | 2001
- 231
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FULL-LENGTH PAPERS - Response Surface Method for Airfoil Design in Transonic FlowAhn, J. et al. | 2001
- 239
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NavierStokes Computations of Limit-Cycle Oscillations for a B-1-Like ConfigurationPeter M. Hartwich / Steven K. Dobbs / Alan E. Arslan / Suk C. Kim et al. | 2001
- 239
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FULL-LENGTH PAPERS - Navier-Stokes Computations of Limit-Cycle Oscillations for a B-1-Like ConfigurationHartwich, P.M. et al. | 2001
- 248
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FULL-LENGTH PAPERS - Suppression of Pressure Oscillations in High-Mach-Number, Turbulent, Cavity FlowPerng, S.W. et al. | 2001
- 248
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Suppression of Pressure Oscillations in High-Mach-Number, Turbulent, Cavity FlowS. W. Perng / D. S. Dolling et al. | 2001
- 257
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Euler Solutions for Airfoils in Inhomogeneous Atmospheric FlowsCaroline Weish-aring / upl / Boris Laschka et al. | 2001
- 257
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FULL-LENGTH PAPERS - Euler Solutions for Airfoils in Inhomogeneous Atmospheric FlowsWeishäupl, C. et al. | 2001
- 266
-
Influence of Yaw Cards on the Yaw Growth of Spin-Stabilized ProjectilesG. R. Cooper et al. | 2001
- 266
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FULL-LENGTH PAPERS - Influence of Yaw Cards on the Yaw Growth of Spin-Stabilized ProjectilesCooper, G.R. et al. | 2001
- 271
-
Exhaust Ducting Effects on Takeoff Lift Loss of Two-Dimensional Hypersonic ConfigurationRobert E. Bond / Gary J. Morris / John L. Loth et al. | 2001
- 271
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FULL-LENGTH PAPERS - Exhaust Ducting Effects on Takeoff Lift Loss of Two-Dimensional Hypersonic ConfigurationBond, R.E. et al. | 2001
- 277
-
Flight Test of Active Structural Acoustic Noise Control SystemDan Palumbo / Ran Cabell / Brenda Sullivan / John Cline et al. | 2001
- 277
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FULL-LENGTH PAPERS - Flight Test of Active Structural Acoustic Noise Control SystemPalumbo, D. et al. | 2001
- 285
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Aerodynamic Simulations of Airfoils with Upper-Surface Ice-ShapesSatish Kumar / Eric Loth et al. | 2001
- 285
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FULL-LENGTH PAPERS - Aerodynamic Simulations of Airfoils with Upper-Surface Ice-ShapesKumar, S. et al. | 2001
- 296
-
FULL-LENGTH PAPERS - Effect of Compressibility on Suppression of Dynamic Stall Using a Slotted AirfoilCarr, L.W. et al. | 2001
- 296
-
Effect of Compressibility on Suppression of Dynamic Stall Using a Slotted AirfoilL. W. Carr / M. S. Chandrasekhara / M. C. Wilder / K. W. Noonan et al. | 2001
- 310
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FULL-LENGTH PAPERS - Aspects of Ground Facility Interference on Leading-Edge Vortex BreakdownEricsson, L.E. et al. | 2001
- 310
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Aspects of Ground Facility Interference on Leading-Edge Vortex BreakdownLars E. Ericsson / Martin E. Beyers et al. | 2001
- 315
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FULL-LENGTH PAPERS - Near-Wake Measurements of a Delta Wing in a Supersonic StreamMilanovic, I.M. et al. | 2001
- 315
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Near-Wake Measurements of a Delta Wing in a Supersonic StreamIvana M. Milanovic / Iraj M. Kalkhoran et al. | 2001
- 326
-
Aerodynamic Drag Prediction of Helicopter FuselageA. Filippone / J. A. Michelsen et al. | 2001
- 326
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FULL-LENGTH PAPERS - Aerodynamic Drag Prediction of Helicopter FuselageFilippone, A. et al. | 2001
- 334
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Calculation of Wing Flutter by a Coupled Fluid-Structure MethodF. Liu / J. Cai / Y. Zhu / H. M. Tsai / A. S. F. Wong et al. | 2001
- 334
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FULL-LENGTH PAPERS - Calculation of Wing Flutter by a Coupled Fluid-Structure MethodLiu, F. et al. | 2001
- 343
-
Aeroelastic Characteristics of Double-Swept Isotropic and Composite WingsKyo-Nam Koo et al. | 2001
- 343
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FULL-LENGTH PAPERS - Aeroelastic Characteristics of Double-Swept Isotropic and Composite WingsKoo, K.-N. et al. | 2001
- 349
-
Numerical Simulation of Dynamically Deforming Aircraft Configurations Using Overset GridsYuval Levy et al. | 2001
- 349
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FULL-LENGTH PAPERS - Numerical Simulation of Dynamically Deforming Aircraft Configurations Using Overset GridsLevy, Y. et al. | 2001
- 355
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Flutter Prediction from Flight Flutter Test DataG. Dimitriadis / J. E. Cooper et al. | 2001
- 355
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FULL-LENGTH PAPERS - Flutter Prediction from Flight Flutter Test DataDimitriadis, G. et al. | 2001
- 368
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Buffet Alleviation on Swept and Unswept Wings at High IncidenceG. A. Flynn / J. F. Morrison / D. G. Mabey et al. | 2001
- 368
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FULL-LENGTH PAPERS - Buffet Alleviation on Swept and Unswept Wings at High IncidenceFlynn, G.A. et al. | 2001
- 379
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FULL-LENGTH PAPERS - Analytical-Experimental Correlation for a Stiffened Composite Panel Loaded in Axial CompressionPark, O. et al. | 2001
- 379
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Analytical-Experimental Correlation for a Stiffened Composite Panel Loaded in Axial CompressionOung Park / Raphael T. Haftka / Bhavani V. Sankar / James H. Starnes / Somanath Nagendra et al. | 2001
- 388
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ENGINEERING NOTES - Simple Loitering Flight Path for High Altitude Uncrewed Aerial VehiclesWeihs, D. et al. | 2001
- 388
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Simple Loitering Flight Path for High Altitude Uncrewed Aerial VehiclesDaniel Weihs et al. | 2001
- 389
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ENGINEERING NOTES - Baseline Validation of Unstructured Grid Reynolds-Averaged Navier-Stokes Toward Flow ControlJoslin, R.D. et al. | 2001
- 389
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Baseline Validation of Unstructured Grid Reynolds-Averaged NavierStokes Toward Flow ControlRonald D. Joslin / Sally A. Viken et al. | 2001
- 393
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Modeling of the Receiver Aircraft in Air-To-Air RefuelingA. W. Bloy / M. M. Khan et al. | 2001
- 393
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ENGINEERING NOTES - Modeling of the Receiver Aircraft in Air-To-Air RefuelingBloy, A.W. et al. | 2001
- 396
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ENGINEERING NOTES - Studies on Vortex Flaps Having Different Flap Hinge-Line PositionsRinoie, K. et al. | 2001
- 396
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Studies on Vortex Flaps Having Different Flap Hinge-Line PositionsKenichi Rinoie / Dong Youn Kwak et al. | 2001
- 398
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ENGINEERING NOTES - Performance Improvements of a Biplane with EndplatesAhmed, N.A. et al. | 2001
- 398
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Performance Improvements of a Biplane with EndplatesN. A. Ahmed / R. D. Archer et al. | 2001
- 401
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Active Flow ControlBright Prospects and Basic Challenges| 2001
- 401
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FLOW CONTROL - Active Flow Control -- Bright Prospects and Basic Challenges| 2001
- 402
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Flow Control: The FutureMohamed Gad-el-Hak et al. | 2001
- 402
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FLOW CONTROL - Flow Control: The FutureGad-el-Hak, M. et al. | 2001
- 419
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Micro-Air-Vehicles: Can They be Controlled Better?Mohamed Gad-el-Hak et al. | 2001
- 430
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Dynamic Stall Control by Periodic Excitation, Part 1: NACA 0015 Parametric StudyD. Greenblatt / I. Wygnanski et al. | 2001
- 430
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FLOW CONTROL - Dynamic Stall Control by Periodic Excitation, Part 1: NACA 0015 Parametric StudyGreenblatt, D. et al. | 2001
- 439
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FLOW CONTROL - Dynamic Stall Control by Periodic Excitation, Part 2: MechanismsGreenblatt, D. et al. | 2001
- 439
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Dynamic Stall Control by Periodic Excitation, Part 2: MechanismsD. Greenblatt / B. Nishri / A. Darabi / I. Wygnanski et al. | 2001
- 448
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FLOW CONTROL - Compressible Dynamic Stall Control: Comparison of Two ApproachesChandrasekhara, M.S. et al. | 2001
- 448
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Compressible Dynamic Stall Control: Comparison of Two ApproachesM. S. Chandrasekhara / M. C. Wilder / L. W. Carr et al. | 2001
- 454
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FLOW CONTROL - Microblowing for High-Angle-of-Attack Vortex Flow Control on a Fighter AircraftRoos, F.W. et al. | 2001
- 454
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Microblowing for High-Angle-of-Attack Vortex Flow Control on a Fighter AircraftFrederick W. Roos et al. | 2001
- 458
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FLOW CONTROL - Numerical Simulation of Enhanced Mixing in Jet Plumes Using Pulsed BlowingSmith, T.D. et al. | 2001
- 458
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Numerical Simulation of Enhanced Mixing in Jet Plumes Using Pulsed BlowingTimothy D. Smith / Alan B. Cain / Clarence F. Chenault et al. | 2001
- 464
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Oscillatory Control of Shock-Induced SeparationAvi Seifert / Latunia G. Pack et al. | 2001
- 464
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FLOW CONTROL - Oscillatory Control of Shock-Induced SeparationSeifert, A. et al. | 2001
- 473
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FLOW CONTROL - A Study of Rotor Tip Vortex Structure Alteration TechniquesLiu, Z. et al. | 2001
- 473
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A Study of Rotor Tip Vortex Structure Alteration TechniquesZhijian Liu / Justin W. Russell / Lakshmi N. Sankar / Ahmed A. Hassan et al. | 2001
- 478
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Applications of Zero-Net-Mass Jets for Enhanced Rotorcraft Aerodynamic PerformanceAhmed A. Hassan et al. | 2001
- 478
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FLOW CONTROL - Applications of Zero-Net-Mass Jets for Enhanced Rotorcraft Aerodynamic PerformanceHassan, A.A. et al. | 2001
- 478
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Applications of Zero-Net-Mass Jets for Enhanced Rotocraft Aerodynamic PerformanceHassan, A. A. et al. | 2001
- 485
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ANNOUNCEMENT - Call for Award Nominations| 2001
- 486
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Periodic Excitation for Jet Vectoring and Enhanced SpreadingLatunia G. Pack / Avi Seifert et al. | 2001
- 496
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Flow Separation Control with Microflexural Wall VibrationsSumon K. Sinha et al. | 2001
- 496
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FLOW CONTROL - Flow Separation Control with Microflexural Wall VibrationsSinha, S.K. et al. | 2001
- 504
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Progress on the Use of Compliant Walls for Laminar-Flow ControlPeter W. Carpenter / Anthony D. Lucey / Christopher Davies et al. | 2001
- 504
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FLOW CONTROL - Progress on the Use of Compliant Walls for Laminar-Flow ControlCarpenter, P.W. et al. | 2001
- 513
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Computational Analysis of Centrifugal Compressor Surge Control Using Air InjectionAlexander Stein / Saeid Niazi / Lakshmi N. Sankar et al. | 2001
- 513
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FLOW CONTROL - Computational Analysis of Centrifugal Compressor Surge Control Using Air InjectionStein, A. et al. | 2001
- 521
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Investigation of a Circulation Controlled Cylinder Using an Adaptive Wall Wind TunnelFabrizio A. Dionisio / Alan Nurick et al. | 2001
- 528
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Experimental Investigation of a Helicopter Circulation-Controlled Tail BoomAlan Nurick et al. | 2001
- 536
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Theoretical and Experimental Investigation of Biplane Delta WingsLance W. Traub et al. | 2001
- 536
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FULL-LENGTH PAPERS - Theoretical and Experimental Investigation of Biplane Delta WingsTraub, L.W. et al. | 2001
- 547
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Efficient Aeroelastic Analysis Using Computational Unsteady AerodynamicsDaniella E. Raveh / Yuval Levy / Moti Karpel et al. | 2001
- 547
-
FULL-LENGTH PAPERS - Efficient Aeroelastic Analysis Using Computational Unsteady AerodynamicsRaveh, D.E. et al. | 2001
- 557
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Flutter Prediction Methods for Aeroelastic Design OptimizationR. M. V. Pidaparti / V. A. Tischler / V. B. Venkayya et al. | 2001
- 557
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FULL-LENGTH PAPERS - Flutter Prediction Methods for Aeroelastic Design OptimizationPidaparti, R.M.V. et al. | 2001
- 560
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FULL-LENGTH PAPERS - Material-Geometry Adaptive Shape Functions for Rayleigh-Ritz Vibration Analysis of Composite PlatesKim, J.-E. et al. | 2001
- 560
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Material/Geometry Adaptive Shape Functions for RayleighRitz Vibration Analysis of Composite PlatesJong-Eun Kim / Nesrin Sarigul-Klijn et al. | 2001
- 565
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Preliminary Results of BE-1900D Operational Flight Loads Data EvaluationThomas A. Zeiler / Daniel O. Tipps / Donald A. Skinn / John W. Rustenburg et al. | 2001
- 565
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FULL-LENGTH PAPERS - Preliminary Results of BE-1900D Operational Flight Loads Data EvaluationZeiler, T.A. et al. | 2001
- 573
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Physical Analysis and Scaling of a Jet and Vortex Actuator (EN)Lachowicz, J. T. / Yao, C.-S. / Joslin, R. D. et al. | 2001
- 573
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FLOW CONTROL - Physical Analysis and Scaling of a Jet and Vortex Actuator (EN)Lachowicz, J.T. et al. | 2001
- 573
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Physical Analysis and Scaling of a Jet and Vortex ActuatorJason T. Lachowicz / Chung-Sheng Yao / Ronald D. Joslin et al. | 2001
- 575
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ENGINEERING NOTES - Sensing Aircraft Icing Effects by Unsteady Flap Hinge-Moment MeasurementGurbacki, H.M. et al. | 2001
- 575
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Sensing Aircraft Icing Effects by Unsteady Flap Hinge-Moment MeasurementHolly M. Gurbacki / Michael B. Bragg et al. | 2001
- 577
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Flow Quality Improvements in a Blowdown Wind TunnelH. Sundara Murthy / R. S. Verma / S. P. Jagadeeswarachar / Rajan Kumar et al. | 2001
- 577
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ENGINEERING NOTES - Flow Quality Improvements in a Blowdown Wind TunnelMurthy, H.S. et al. | 2001
- 580
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Concise Orthogonal Representation of Supercritical AirfoilsG. M. Robinson / A. J. Keane et al. | 2001
- 580
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ENGINEERING NOTES - Concise Orthogonal Representation of Supercritical AirfoilsRobinson, G.M. et al. | 2001
- 583
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Effect of Tip Vortex Geometry on the Flow Through the Blades of Hovering RotorsD. H. Wood et al. | 2001
- 583
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ENGINEERING NOTES - Effect of Tip Vortex Geometry on the Flow Through the Blades of Hovering RotorsWood, D.H. et al. | 2001
- 584
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Divergence and the p-k Flutter EquationLouw H. van Zyl / Motodi S. Maserumule et al. | 2001
- 584
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ENGINEERING NOTES - Divergence and the p-k Flutter EquationZyl, L.H.van et al. | 2001
- 586
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Aeroelastic Divergence and Aerodynamic Lag RootsLouw H. van Zyl et al. | 2001
- 586
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ENGINEERING NOTES - Aeroelastic Divergence and Aerodynamic Lag RootsZyl, L.H.van et al. | 2001
- 588
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Unrestrained Aeroelastic Divergence and the p-k Flutter EquationLouw H. van Zyl / Motodi S. Maserumule et al. | 2001
- 588
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ENGINEERING NOTES - Unrestrained Aeroelastic Divergence and the p-k Flutter EquationZyl, L.H.van et al. | 2001
- 590
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Simplified Treatment of Unsteady Aerodynamics for Lifting RotorsR. H. Miller et al. | 2001
- 590
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ENGINEERING NOTES - Simplified Treatment of Unsteady Aerodynamics for Lifting RotorsMiller, R.H. et al. | 2001
- 593
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FULL-LENGTH PAPERS - Probability of Collision of Aircraft with Dissimilar Position ErrorsCampos, L.M.B.C. et al. | 2001
- 593
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Probability of Collision of Aircraft with Dissimilar Position ErrorsL. M. B. C. Campos et al. | 2001
- 600
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FULL-LENGTH PAPERS - Evaluation of Perceived Motion During a Simulated Takeoff RunGroen, E.L. et al. | 2001
- 600
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Evaluation of Perceived Motion During a Simulated Takeoff RunEric L. Groen / Mario S. V. Valenti Clari / Ruud J. A. W. Hosman et al. | 2001
- 607
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Assessment of Flight Simulator Fidelity in Multiaxis Tasks Including Visual Cue QualityR. A. Hess / W. Siwakosit et al. | 2001
- 607
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FULL-LENGTH PAPERS - Assessment of Flight Simulator Fidelity in Multiaxis Tasks Including Visual Cue QualityHess, R.A. et al. | 2001
- 615
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FULL-LENGTH PAPERS - Maneuvering in Mountains on the Back Side of the Banked Power CurveLowry, J.T. et al. | 2001
- 615
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Maneuvering in Mountains on the Back Side of the Banked Power CurveJohn T. Lowry et al. | 2001
- 620
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Optimization of Noise Abatement Departure TrajectoriesH. G. Visser / R. A. A. Wijnen et al. | 2001
- 620
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FULL-LENGTH PAPERS - Optimization of Noise Abatement Departure TrajectoriesVisser, H.G. et al. | 2001
- 628
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FULL-LENGTH PAPERS - CFD-Based Aeroelastic Eigensolver for the Subsonic, Transonic, and Supersonic RegimesLesoinne, M. et al. | 2001
- 628
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CFD-Based Aeroelastic Eigensolver for the Subsonic, Transonic, and Supersonic RegimesMichel Lesoinne / Charbel Farhat et al. | 2001
- 636
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Numerical Simulation of Aircraft Trailing Vortices Interacting with Ambient Shear or GroundM. Mokry et al. | 2001
- 636
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FULL-LENGTH PAPERS - Numerical Simulation of Aircraft Trailing Vortices Interacting with Ambient Shear or GroundMokry, M. et al. | 2001
- 644
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Inverse Design of Transonic Wings Using Wing Planform and Target Pressure OptimizationTaisul Ahn / Hyoung-Jin Kim / Chongam Kim / Oh-Hyun Rho et al. | 2001
- 644
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FULL-LENGTH PAPERS - Inverse Design of Transonic Wings Using Wing Planform and Target Pressure OptimizationAhn, T. et al. | 2001
- 653
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FULL-LENGTH PAPERS - Control Surface Reversal in the Transonic Regime Including Viscous EffectsEastep, F. et al. | 2001
- 653
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Control Surface Reversal in the Transonic Regime Including Viscous EffectsF. Eastep / G. Andersen / P. Beran / R. Kolonay et al. | 2001
- 664
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FULL-LENGTH PAPERS - Multidisciplinary Design of Vehicle Structures with Improved Roll Maneuverability -- Transonic RegimeAryasomayajula, S. et al. | 2001
- 664
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Multidisciplinary Design of Vehicle Structures with Improved Roll ManeuverabilityTransonic RegimeS. Aryasomayajula / H. Wang / R. Grandhi / F. Eastep et al. | 2001
- 672
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Euler Computations of Rotor Flows on Unstructured Rotating MeshesDartzi Pan / Maw-Jyi Chao / S. K. Chien et al. | 2001
- 672
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FULL-LENGTH PAPERS - Euler Computations of Rotor Flows on Unstructured Rotating MeshesPan, D. et al. | 2001
- 680
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Hypersonic Drag and Heat-Transfer Reduction Using a Forward-Facing JetBenjamin Meyer / H. F. Nelson / David W. Riggins et al. | 2001
- 680
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FULL-LENGTH PAPERS - Hypersonic Drag and Heat-Transfer Reduction Using a Forward-Facing JetMeyer, B. et al. | 2001
- 687
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Wake-Vortex Eddy-Dissipation Model Predictions Compared with ObservationsT. Sarpkaya / R. E. Robins / D. P. Delisi et al. | 2001
- 687
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FULL-LENGTH PAPERS - Wake-Vortex Eddy-Dissipation Model Predictions Compared with ObservationsSarpkaya, T. et al. | 2001
- 693
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Transonic Flow of Moist Air Around a Thin Airfoil with Equilibrium CondensationJang-Chang Lee / Zvi Rusak et al. | 2001
- 693
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FULL-LENGTH PAPERS - Transonic Flow of Moist Air Around a Thin Airfoil with Equilibrium CondensationLee, J.-C. et al. | 2001
- 703
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FULL-LENGTH PAPERS - Experimental Investigation of Multielement Airfoil Lift Hysteresis due to Flap RiggingLandman, D. et al. | 2001
- 703
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Experimental Investigation of Multielement Airfoil Lift Hysteresis due to Flap RiggingDrew Landman / Colin P. Britcher et al. | 2001
- 709
-
Flap-Deflection Optimization for Transonic Cruise Performance Improvement of Supersonic Transport WingHyoung-Jin Kim / Shigeru Obayashi / Kazuhiro Nakahashi et al. | 2001
- 709
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FULL-LENGTH PAPERS - Flap-Deflection Optimization for Transonic Cruise Performance Improvement of Supersonic Transport WingKim, H.-J. et al. | 2001
- 718
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Review of Attitude Representations Used for Aircraft KinematicsW. F. Phillips / C. E. Hailey / G. A. Gebert et al. | 2001
- 718
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FULL-LENGTH PAPERS - Review of Attitude Representations Used for Aircraft KinematicsPhillips, W.F. et al. | 2001
- 738
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Three-Dimensional Gore Design Concept for High-Pressure BalloonsNobuyuki Yajima / Naoki Izutsu / Hideyuki Honda / Haruhisa Kurokawa / Kiyoho Matsushima et al. | 2001
- 738
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FULL-LENGTH PAPERS - Three-Dimensional Gore Design Concept for High-Pressure BalloonsYajima, N. et al. | 2001
- 745
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FULL-LENGTH PAPERS - Videogrammetric Model Deformation Measurement TechniqueBurner, A.W. et al. | 2001
- 745
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Videogrammetric Model Deformation Measurement TechniqueA. W. Burner / Tianshu Liu et al. | 2001
- 755
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Accurate Subcritical Damping Solution of Flutter Equation Using Piecewise Aerodynamic FunctionCharles Goodman et al. | 2001
- 755
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FULL-LENGTH PAPERS - Accurate Subcritical Damping Solution of Flutter Equation Using Piecewise Aerodynamic FunctionGoodman, C. et al. | 2001
- 764
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FULL-LENGTH PAPERS - Strength of Stiffened 2024-T3 Aluminum Panels with Multiple Site DamageSmith, B.L. et al. | 2001
- 764
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Strength of Stiffened 2024-T3 Aluminum Panels with Multiple Site DamageB. L. Smith / A. L. Hijazi / A. K. M. Haque / R. Y. Myose et al. | 2001
- 769
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Computational Study of the High-Lift A-AirfoilAdam Jir-Uuml / sek / Peter Eliasson / Stefan Wallin et al. | 2001
- 769
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ENGINEERING NOTES - Computational Study of the High-Lift A-AirfoilJirásek, A. et al. | 2001
- 772
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Improving the Convergence of the Doublet-Lattice Method Through Tip CorrectionsMyles L. Baker / William P. Rodden et al. | 2001
- 772
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ENGINEERING NOTES - Improving the Convergence of the Doublet-Lattice Method Through Tip CorrectionsBaker, M.L. et al. | 2001
- 776
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Parametric Study of the PhugoidS. Pradeep et al. | 2001
- 776
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ENGINEERING NOTES - Parametric Study of the PhugoidPradeep, S. et al. | 2001
- 778
-
ENGINEERING NOTES - Wave Drag Estimation for Use with Panel CodesPetruzzelli, N. et al. | 2001
- 778
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Wave Drag Estimation for Use with Panel CodesN. Petruzzelli / A. J. Keane et al. | 2001
- 783
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ERRATA - Active Flow Control -- Bright Prospects and Basic ChallengesMcMichael, J. et al. | 2001
- 784
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ERRATA - Wing Rock of Nonslender Delta WingsEricsson, L.E. et al. | 2001
- 785
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AERODYNAMIC DECELERATOR SYSTEMS - Aerodynamic Decelerator Systems -- Diverse Challenges and Recent AdvancesBenney, R. et al. | 2001
- 785
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Aerodynamic Decelerator SystemsDiverse Challenges and Recent AdvancesRichard Benney / Michael Accorsi et al. | 2001
- 786
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Flight Testing the Parachute System for the Space Station Crew Return VehicleRicardo A. Mach-egrave / n / Christie S. Iacomini / Chris J. Cerimele / Jenny M. Stein et al. | 2001
- 786
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AERODYNAMIC DECELERATOR SYSTEMS - Flight Testing the Parachute System for the Space Station Crew Return VehicleMachin, R.A. et al. | 2001
- 800
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Fluid-Structure Interactions of a Round Parachute: Modeling and Simulation TechniquesKeith R. Stein / Richard J. Benney / Tayfun E. Tezduyar / John W. Leonard / Michael L. Accorsi et al. | 2001
- 800
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AERODYNAMIC DECELERATOR SYSTEMS - Fluid-Structure Interactions of a Round Parachute: Modeling and Simulation TechniquesStein, K.R. et al. | 2001
- 809
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AERODYNAMIC DECELERATOR SYSTEMS - Guidance and Control for Flat-Circular ParachutesDellicker, S. et al. | 2001
- 809
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Guidance and Control for Flat-Circular ParachutesScott Dellicker / Richard Benney / Glen Brown et al. | 2001
- 818
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Modeling the Inflation of Ram-Air Parachutes Reefed with SlidersJ. Potvin / G. Peek / B. Brocato et al. | 2001
- 818
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AERODYNAMIC DECELERATOR SYSTEMS - Modeling the Inflation of Ram-Air Parachutes Reefed with SlidersPotvin, J. et al. | 2001
- 828
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Analysis of a Boeing 747 Aircraft Fuel Tank Vent SystemD. L. Jensen et al. | 2001
- 828
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FULL-LENGTH PAPERS - Analysis of a Boeing 747 Aircraft Fuel Tank Vent SystemJensen, D.L. et al. | 2001
- 835
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FULL-LENGTH PAPERS - Hybrid-System Simulation for National Airspace System Safety AnalysisPritchett, A.R. et al. | 2001
- 835
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Hybrid-System Simulation for National Airspace System Safety AnalysisA. R. Pritchett / S. M. Lee / D. Goldsman et al. | 2001
- 841
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FULL-LENGTH PAPERS - F-A-18E-F Super Hornet High-Angle-of-Attack Control Law Development and TestingHeller, M. et al. | 2001
- 841
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F/A-18E/F Super Hornet High-Angle-of-Attack Control Law Development and TestingMichael Heller / Robert J. Niewoehner / Kenneth P. Lawson et al. | 2001
- 848
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Nested Fork-Join Queueing Network Model for Analysis of Airfield OperationsCraig J. Willits / Dennis C. Dietz et al. | 2001
- 848
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FULL-LENGTH PAPERS - Nested Fork-Join Queueing Network Model for Analysis of Airfield OperationsWillits, C.J. et al. | 2001
- 856
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FULL-LENGTH PAPERS - Application of the Global Positioning System in Determination of Vehicular AccelerationPinder, S.D. et al. | 2001
- 856
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Application of the Global Positioning System in Determination of Vehicular AccelerationShane D. Pinder / Trever G. Crowe / Peter N. Nikiforuk et al. | 2001
- 860
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FULL-LENGTH PAPERS - Multipoint Aerodynamic Wing Optimization in Viscous FlowSzmelter, J. et al. | 2001
- 860
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Multipoint Aerodynamic Wing Optimization in Viscous FlowJ. Szmelter et al. | 2001
- 868
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FULL-LENGTH PAPERS - Effect of Wake Adaptation on Rotor Hover Simulations Using Unstructured MeshesKang, H.J. et al. | 2001
- 868
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Effect of Wake Adaptation on Rotor Hover Simulations Using Unstructured MeshesHee Jung Kang / Oh Joon Kwon et al. | 2001
- 878
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FULL-LENGTH PAPERS - On the Structure and Attenuation of an Aircraft WakeÖzger, E. et al. | 2001
- 878
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On the Structure and Attenuation of an Aircraft WakeE. -Oslash / zger / I. Schell / D. Jacob et al. | 2001
- 888
-
Parametric Study of Transient Spoiler Aerodynamics with Two-Equation Turbulence ModelsSeong-Wook Choi / Keun-Shik Chang / Honam Ok et al. | 2001
- 888
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FULL-LENGTH PAPERS - Parametric Study of Transient Spoiler Aerodynamics with Two-Equation Turbulence ModelsChoi, S.-W. et al. | 2001
- 895
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Three-Dimensional NavierStokes Simulations for Transport Aircraft High-Lift ConfigurationsR. Rudnik / S. Melber / A. Ronzheimer / O. Brodersen et al. | 2001
- 895
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FULL-LENGTH PAPERS - Three-Dimensional Navier -- Stokes Simulations for Transport Aircraft High-Lift ConfigurationsRudnik, R. et al. | 2001
- 904
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Recent Turbulence Model Advances Applied to Multielement Airfoil ComputationsChristopher L. Rumsey / Thomas B. Gatski et al. | 2001
- 904
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FULL-LENGTH PAPERS - Recent Turbulence Model Advances Applied to Multielement Airfoil ComputationsRumsey, C.L. et al. | 2001
- 911
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Algorithm for Prediction of Trailing Vortex EvolutionRobert E. Robins / Donald P. Delisi / George C. Greene et al. | 2001
- 911
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FULL-LENGTH PAPERS - Algorithm for Prediction of Trailing Vortex EvolutionRobins, R.E. et al. | 2001
- 918
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Efficient Inverse Aerodynamic Design Method for Subsonic FlowsWilliam E. Milholen et al. | 2001
- 918
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FULL-LENGTH PAPERS - Efficient Inverse Aerodynamic Design Method for Subsonic FlowsMilholen II, W.E. et al. | 2001
- 924
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Jet/Intake Interference in Short Take off, Vertical Landing AircraftA. J. Saddington / K. Knowles et al. | 2001
- 924
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FULL-LENGTH PAPERS - Jet-Intake Interference in Short Take off, Vertical Landing AircraftSaddington, A.J. et al. | 2001
- 932
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FULL-LENGTH PAPERS - Flow Physics Generating Highly Nonlinear Lateral Stability Characteristics of a 65-Degree Delta-Wing-BodyEricsson, L.E. et al. | 2001
- 932
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Flow Physics Generating Highly Nonlinear Lateral Stability Characteristics of 65-Degree Delta-WingBodyLars E. Ericsson et al. | 2001
- 932
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Flow Physics Generating Highly Nonlinear Lateral Stability Characteristics of a 65-Degree Delta-Wing-BodyEricsson, L. E. et al. | 2001
- 935
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Development and Evaluation of a Cockpit Decision-Aid for Emergency Trajectory GenerationTed L. Chen / Amy R. Pritchett et al. | 2001
- 935
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FULL-LENGTH PAPERS - Development and Evaluation of a Cockpit Decision-Aid for Emergency Trajectory GenerationChen, T.L. et al. | 2001
- 944
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Correction of Wall Interference in Wind Tunnels: A Numerical InvestigationGiovanni Lombardi / Maria Vittoria Salvetti / Mauro Morelli et al. | 2001
- 944
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FULL-LENGTH PAPERS - Correction of Wall Interference in Wind Tunnels: A Numerical InvestigationLombardi, G. et al. | 2001
- 950
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Evaluation of Scaling Approach for Stiffened Composite Flat Panels Loaded in CompressionMarshall Rouse / Mahyar Assadi et al. | 2001
- 956
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Altitude- and Weight-Scaling Laws for Ram-Air Parachute InflationJ. Potvin et al. | 2001
- 956
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ENGINEERING NOTES - Altitude- and Weight-Scaling Laws for Ram-Air Parachute InflationPotvin, J. et al. | 2001
- 958
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ENGINEERING NOTES - Aeroservoelastic Design Optimization with Experimental VerificationBorglund, D. et al. | 2001
- 958
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Aeroservoelastic Design Optimization with Experimental VerificationDan Borglund et al. | 2001
- 961
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Poststall Behavior of a Wing Under Externally Imposed SoundN. A. Ahmed / R. D. Archer et al. | 2001
- 961
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ENGINEERING NOTES - Poststall Behavior of a Wing Under Externally Imposed SoundAhmed, N.A. et al. | 2001
- 963
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ENGINEERING NOTES - Lift and Drag Characteristics of a Supersonic Biplane ConfigurationTraub, L.W. et al. | 2001
- 963
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Lift and Drag Characteristics of a Supersonic Biplane ConfigurationLance W. Traub et al. | 2001
- 967
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HISTORY - Frank W. Caldwell and Variable-Pitch Propeller Development, 1918-1938Kinney, J.R. et al. | 2001
- 967
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Frank W. Caldwell and Variable-Pitch Propeller Development, 19181938J. R. Kinney et al. | 2001
- 977
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FULL-LENGTH PAPERS - Aircraft Spacings That Produce Vortex-Free Region Below Flight FormationsRossow, V.J. et al. | 2001
- 977
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Aircraft Spacings That Produce Vortex-Free Region Below Flight FormationsVernon J. Rossow et al. | 2001
- 988
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Runway Operations Planning and Control: Sequencing and SchedulingIoannis Anagnostakis / John-Paul Clarke / Dietmar B-ograve / hme / Uwe V-ograve / lcker et al. | 2001
- 988
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FULL-LENGTH PAPERS - Runway Operations Planning and Control: Sequencing and SchedulingAnagnostakis, I. et al. | 2001
- 997
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Single-Point and Multipoint Aerodynamic Shape Optimization of High-Speed Civil TransportSusan E. Cliff / James J. Reuther / David A. Saunders / Raymond M. Hicks et al. | 2001
- 997
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FULL-LENGTH PAPERS - Single-Point and Multipoint Aerodynamic Shape Optimization of High-Speed Civil TransportCliff, S.E. et al. | 2001
- 1006
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Multidisciplinary Design Optimization of a Transonic Commercial Transport with Strut-Braced WingFrank H. Gern / Andy Ko / Erwin Sulaeman / John F. Gundlach / Rakesh K. Kapania / Raphael T. Haftka et al. | 2001
- 1006
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FULL-LENGTH PAPERS - Multidisciplinary Design Optimization of a Transonic Commercial Transport with Strut-Braced WingGern, F.H. et al. | 2001
- 1015
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Novel Multidisciplinary Shape Parameterization ApproachJamshid A. Samareh et al. | 2001
- 1025
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FULL-LENGTH PAPERS - Methodology for Supersonic Panel Flutter Analysis of Thermal Protection System SealsCheng, G. et al. | 2001
- 1025
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Methodology for Supersonic Panel Flutter Analysis of Thermal Protection System SealsGuangfeng Cheng / Chuh Mei / Roger R. Chen et al. | 2001
- 1032
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FULL-LENGTH PAPERS - Assessing Computational Fluid Dynamics Predictions for Control Surface EffectivenessJiang, F. et al. | 2001
- 1032
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Assessing Computational Fluid Dynamics Predictions for Control Surface EffectivenessFeng Jiang et al. | 2001
- 1040
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Perturbations of a Delta Wing: Control of Vortex Breakdown and BuffetingM. -Oslash / zg-ograve / ren, B. Sahin / D. Rockwell et al. | 2001
- 1051
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Study of Transition in a High-Disturbance EnvironmentR. D. McDaniel / H. A. Hassan et al. | 2001
- 1051
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FULL-LENGTH PAPERS - Study of Transition in a High-Disturbance EnvironmentMcDaniel, R.D. et al. | 2001
- 1056
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FULL-LENGTH PAPERS - Effect of Endplates on Two-Dimensional Airfoil Testing at Low Reynolds NumberPelletier, A. et al. | 2001
- 1056
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Effect of Endplates on Two-Dimensional Airfoil Testing at Low Reynolds NumberAlain Pelletier / Thomas J. Mueller et al. | 2001
- 1060
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Computation of Viscous Flow for a Boeing 777 Aircraft in Landing ConfigurationStuart E. Rogers / Karlin Roth / Hoa V. Cao / Jeffrey P. Slotnick / Mark Whitlock / Steven M. Nash / M. David Baker et al. | 2001
- 1060
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FULL-LENGTH PAPERS - Computation of Viscous Flow for a Boeing 777 Aircraft in Landing ConfigurationRogers, S.E. et al. | 2001
- 1069
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Experimental Validation of the Wing Dihedral Effect Using a Whirling Arm EquipmentPiero A. Gili / Manuela Battipede et al. | 2001
- 1069
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FULL-LENGTH PAPERS - Experimental Validation of the Wing Dihedral Effect Using a Whirling Arm EquipmentGili, P.A. et al. | 2001
- 1076
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Design-Oriented High-Lift Methodology for General Aviation and Civil Transport AircraftC. P. van Dam / J. C. Vander Kam / J. K. Paris et al. | 2001
- 1076
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FULL-LENGTH PAPERS - Design-Oriented High-Lift Methodology for General Aviation and Civil Transport AircraftDam, C.P.van et al. | 2001
- 1085
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Numerical Determination of Circulation for a Swept PropellerM. Tremmel / D. B. Taulbee / J. R. Sonnenmeier et al. | 2001
- 1085
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FULL-LENGTH PAPERS - Numerical Determination of Circulation for a Swept PropellerTremmel, M. et al. | 2001
- 1093
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FULL-LENGTH PAPERS - Approximation and Model Management in Aerodynamic Optimization with Variable-Fidelity ModelsAlexandrov, N.M. et al. | 2001
- 1093
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Approximation and Model Management in Aerodynamic Optimization with Variable-Fidelity ModelsNatalia M. Alexandrov / Robert Michael Lewis / Clyde R. Gumbert / Lawrence L. Green / Perry A. Newman et al. | 2001
- 1102
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FULL-LENGTH PAPERS - Impulsively Started Flow About a Rigid Parachute CanopyJohari, H. et al. | 2001
- 1102
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Impulsively Started Flow About a Rigid Parachute CanopyH. Johari / K. Stein / T. Tezduyar et al. | 2001
- 1110
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Streamlining Flight Test with the Design and Analysis of ExperimentsJames R. Simpson / James W. Wisnowski et al. | 2001
- 1110
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FULL-LENGTH PAPERS - Streamlining Flight Test with the Design and Analysis of ExperimentsSimpson, J.R. et al. | 2001
- 1117
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Rocket-Based Combined-Cycle Engine Integration on an Osculating Cone Waverider VehicleTimothy F. O&apos / Brien / Mark J. Lewis et al. | 2001
- 1117
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FULL-LENGTH PAPERS - Rocket-Based Combined-Cycle Engine Integration on an Osculating Cone Waverider VehicleO'Brien, T.F. et al. | 2001
- 1124
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Comparison of Visually Coupled System Performance in Helicopter Flight and Simulator TrialsSion Jennings / Lloyd Reid / Eric Tai et al. | 2001
- 1124
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FULL-LENGTH PAPERS - Comparison of Visually Coupled System Performance in Helicopter Flight and Simulator TrialsJennings, S. et al. | 2001
- 1130
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FULL-LENGTH PAPERS - Benefits of Swept-and-Leaned Stators for Fan Noise ReductionWoodward, R.P. et al. | 2001
- 1130
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Benefits of Swept-and-Leaned Stators for Fan Noise ReductionRichard P. Woodward / David M. Elliott / Christopher E. Hughes / Jeffrey J. Berton et al. | 2001
- 1139
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FULL-LENGTH PAPERS - Maneuver Trim Optimization Techniques for Active Aeroelastic WingsZink, P.S. et al. | 2001
- 1139
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Maneuver Trim Optimization Techniques for Active Aeroelastic WingsP. Scott Zink / Dimitri N. Mavris / Daniella E. Raveh et al. | 2001
- 1147
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Aeroelastic Deformation Measurements of Flap, Gap, and Overhang on a Semispan ModelA. W. Burner / Tianshu Liu / Sanjay Garg / Terence A. Ghee / Nigel J. Taylor et al. | 2001
- 1147
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FULL-LENGTH PAPERS - Aeroelastic Deformation Measurements of Flap, Gap, and Overhang on a Semispan ModelBurner, A.W. et al. | 2001
- 1155
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2001 JOURNAL OF AIRCRAFT INDEX - Subject Index| 2001
- 1161
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2001 JOURNAL OF AIRCRAFT INDEX - Author Index| 2001
- 1162
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2001 JOURNAL OF AIRCRAFT INDEX - Chronological Index| 2001