Aeroship: A Hybrid Flight Platform (Englisch)
- Neue Suche nach: Liu, T.
- Neue Suche nach: Liu, T.
- Neue Suche nach: Liou, W.W.
- Neue Suche nach: Schulte, M.
In:
Journal of aircraft
;
46
, 2
; 667-674
;
2009
-
ISSN:
- Aufsatz (Zeitschrift) / Print
-
Titel:Aeroship: A Hybrid Flight Platform
-
Beteiligte:
-
Erschienen in:Journal of aircraft ; 46, 2 ; 667-674
-
Verlag:
- Neue Suche nach: Inst.
-
Erscheinungsort:Reston, Va. [u.a.]
-
Erscheinungsdatum:2009
-
ISSN:
-
ZDBID:
-
Medientyp:Aufsatz (Zeitschrift)
-
Format:Print
-
Sprache:Englisch
- Neue Suche nach: 55.50 / 55.50
- Weitere Informationen zu Basisklassifikation
- Neue Suche nach: 770/7040
-
Schlagwörter:
-
Klassifikation:
-
Datenquelle:
Inhaltsverzeichnis – Band 46, Ausgabe 2
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.
- 353
-
ANNOUNCEMENT - New Editor-in-Chief Sought for the Journal of Propulsion and Power| 2009
- 354
-
Prediction of F-16XL Flight-Flow PhysicsLamar, J.E. et al. | 2009
- 354
-
SPECIAL SECTION: PREDICTION OF F-16XL FLIGHT-FLOW PHYSICS - Prediction of F-16XL Flight-Flow PhysicsLamar, J.E. et al. | 2009
- 355
-
Overview of the Cranked-Arrow Wing Aerodynamics Project InternationalObara, C.J. et al. | 2009
- 369
-
F-16XL Geometry and Computational Grids Used in Cranked-Arrow Wing Aerodynamics Project InternationalBoelens, O.J. et al. | 2009
- 377
-
Comparison of Measured and Block Structured Simulation Results for the F-16XL AircraftBoelens, O.J. et al. | 2009
- 385
-
Standard Unstructured Grid Solutions for Cranked Arrow Wing Aerodynamics Project International F-16XLGörtz, S. et al. | 2009
- 409
-
Reynolds-Averaged Navier-Stokes Solutions for the CAWAPI F-16XL Using Different Hybrid GridsFritz, W. et al. | 2009
- 423
-
Lessons Learned from Numerical Simulations of the F-16XL Aircraft at Flight ConditionsRizzi, A. et al. | 2009
- 442
-
Investigation of the Propeller Slipstream with Particle Image VelocimetryRoosenboom, E.W.M. et al. | 2009
- 450
-
Time-Periodic Stability of a Flapping Insect Wing Structure in HoverRosenfeld, N.C. et al. | 2009
- 465
-
Propulsive Force of a Flexible Flapping Thin AirfoilGulcat, U. et al. | 2009
- 474
-
Prediction of UH-60A Structural Loads Using Multibody Analysis and Swashplate DynamicsAbhishek, A. et al. | 2009
- 491
-
Improved Accuracy, Second-Order Response Model for Pressure Sensing SystemsWhitmore, S.A. et al. | 2009
- 501
-
Continuous Disreefing Method for Parachute OpeningSadeck, J.E. et al. | 2009
- 505
-
Lateral Stability of Aircraft Nose-Wheel Landing Gear with Closed-Loop Shimmy DamperSura, N.K. et al. | 2009
- 510
-
Conceptual Design Considerations for Microwave- and Solar-Powered Fuel-Less AircraftWickenheiser, A.M. et al. | 2009
- 520
-
Numerical Study of High-Resolution Scheme Based on Preconditioning MethodXie, F. et al. | 2009
- 526
-
Comparative Study of Three-Dimensional Wing Drag Minimization by Different Optimization TechniquesEpstein, B. et al. | 2009
- 542
-
Aerodynamic Characteristics of Airfoil with Perforated Gurney-Type FlapsLee, T. et al. | 2009
- 549
-
Hydraulic Jump Formation in Water Sloshing Within an Oscillating TankDisimile, P.J. et al. | 2009
- 557
-
New Electric Field Computation Method for AircraftDa, X. et al. | 2009
- 562
-
Ideal Lift Distributions and Flap Angles for Adaptive WingsGopalarathnam, A. et al. | 2009
- 572
-
Characteristic Length and Dynamic Time Scale Associated with Aircraft Pitching MotionPhillips, W.F. et al. | 2009
- 583
-
Optimization of Flapping Motion Parameters for Two Airfoils in a Biplane ConfigurationKaya, M. et al. | 2009
- 593
-
Supersonic Flutter of Functionally Graded Panels Subject to Acoustic and Thermal LoadsIbrahim, H.H. et al. | 2009
- 601
-
Design of Composite Wings Including Uncertainties: A Probabilistic ApproachManan, A. et al. | 2009
- 608
-
Graphical Techniques for Managing Field Failures of Aircraft Systems and ComponentsAl-Garni, A.Z. et al. | 2009
- 617
-
Computational Modeling of Variable-Droop Leading Edge in Forward FlightBain, J.J. et al. | 2009
- 627
-
Three-Dimensional Trajectory Optimization in Constrained AirspaceDai, R. et al. | 2009
- 635
-
Robust Aerodynamic Design Optimization Using Polynomial ChaosDodson, M. et al. | 2009
- 647
-
Experimental Investigation of Bistable Winglets to Enhance Wing Lift Takeoff CapabilityGatto, A. et al. | 2009
- 656
-
Numerical and Experimental Analysis of a Generic Fan-in-Wing ConfigurationThouault, N. et al. | 2009
- 667
-
Aeroship: A Hybrid Flight PlatformLiu, T. et al. | 2009
- 675
-
Numerical and Experimental Validation of Three-Dimensional Shock Control BumpsKönig, B. et al. | 2009
- 683
-
DESIGN FORUM - Pitch Handling Qualities Investigation of the Tailless Gull-Wing ConfigurationAgenbag, D.S. et al. | 2009
- 683
-
Pitch Handling Qualities Investigation of the Tailless Gull-Wing ConfigurationAgenbag, D.S. / Theron, N.J. / Huyssen, R.J. et al. | 2009
- 692
-
Smart Spring Control of Vibration on Helicopter Rotor BladesOxley, G. / Nitzsche, F. / Feszty, D. et al. | 2009
- 692
-
ENGINEERING NOTES - Smart Spring Control of Vibration on Helicopter Rotor BladesOxley, G. et al. | 2009
- 696
-
Stowability Constraint Within a Two-Dimensional Aerodynamic Optimization MethodKolla, M.L. et al. | 2009
- 699
-
Performance, Usage, and Turbofan Transient Simulation Comparisons Between Three Commercial Simulation ToolsGomes, K.J. et al. | 2009
- 705
-
Can Supersonic Transport Be Ultraquiet?Fournier, G.F. et al. | 2009
- 708
-
Comparison of Theoretical Structural Models with Experiment for a High-Aspect-Ratio Aeroelastic WingJaworski, J.W. et al. | 2009
- 713
-
Aircraft Wake Vortex Scenarios Simulation Package for Takeoff and DepartureHolzäpfel, F. et al. | 2009
- 717
-
Vortex Wake Generated Behind a Forward Swept WingLee, T. et al. | 2009
- 721
-
Simulation of Heat Transfer from Hot-Air Jets Impinging a Three-Dimensional Concave SurfaceFregeau, M. et al. | 2009
- 726
-
Wing Planform Design Optimization for Reusable Launch VehicleManokaran, K. et al. | 2009
- 730
-
Promising Benefits of an Active-Extrados Morphing Laminar WingCoutu, D. et al. | 2009
- 731
-
Design of a High-Lift System with Droop Nose DeviceJirásek, A. et al. | 2009