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