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Flugmechanik
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Aircraft Stall Phenomenon Analysis Using Nonlinearity Index Theory
Flight Performance Issues of Electric Aircraft
Analysis of APC Characteristics of Control Mode Switching Induced by Active Side Stick
Solution methods for variational problems of low thrust space flight mechanics
End-To-End Simulation of Launch Vehicle Trajectories Including Stage Separation Dynamics
Adaptive Control of Flow over Wind Turbine Blades
Bifurcation Analysis and Simulation of Stall and Spin Recovery for Large Transport Aircraft
Unsteady Aerodynamic Modeling in Rol for the NASA Generic Transport Model
Debris Aerodynamic Interactions during Uncontrolled Atmospheric Reentry
Gust Response Sensitivity Characteristics of Very Flexible Aircraft
Atmospheric Data System Sensor Placement Optimization for Mars Entry, Descent, and Landing
Simulation Tool for Testing and Validating UAV Autopilots in Wind Gust Environments
Continuous Differentiation of Complex Systems Applied to a Hypersonic Vehicle
Store Separation Equations of Motion
Aerodynamic Parameter Identification for Symmetric Projectiles: An Improved Gradient Based Method
A Two-Stage Method for the Parametric Identification of Scale-Model Helicopter Dynamics
Simulation of Aircraft Encounters with Perturbed Vortices Considering Unsteady Aerodynamic Effects
Modeling and Detection of Ice Particle Accretion in Aircraft Engine Compression Systems
Trim Analysis of a Moving-mass Actuated Airplane
Bifurcation Behaviour of a Flapping Wing MAV in Longitudinal Flight
Guidance algorithms for proximity to target spacecraft
Aerodynamic Effects of Parafoil Upper Surface Bleed Air Actuation
Design Evolution of a High Packing Density Micro Air Vehicle for Local-Area Seeding
Computational 3D Icing Results for Scaled DLR-F6 Geometry
Aircraft Dynamic Modeling in Turbulence
Bifurcation Analysis of the NASA GTM with a View to Upset Recovery
Model-based Aerodynamic-angle Attitude Control of an Atmospheric Entry Capsule
Survey of Blunt Body Dynamic Stability in Supersonic Flow
Center of Gravity Estimation of an Aircraft Solely Using Standard Aircraft Measurement Sensors
Application of Sweet Spot Determination to a Conventional Pair of Aircraft
Helicopter aerodynamics / Ray Prouty ; Volume 3: Ray Prouty's Vertiflite Magazine columns 1990-2013
Effects of Freeplay on Aircraft Main Landing Gear Stability
Real-Time Frequency Response Estimation Using Joined-Wing SensorCraft Aeroelastic Wind-Tunnel Data
Investigation of the Prediction Error Identification for Flutter Prediction
Aerodynamic Model Identification of Frauke UAV
Development of a Fundamental Model for Flapping Wing MAVs and Preliminary Validation
Performance Enhancements by Bounding Flight
System Identification of Flexible Aircraft in Time Domain
Aircraft Spin Phenomenon Analysis Using Nonlinearity Index Theory
Effects of Articulated Wings on the Stability of Small Unmanned Aircraft
Linear, Parameter Varying Model Reduction for Aeroservoelastic Systems
An Initial Flight Investigation of Formation Flight for Drag Reduction on the C-17 Aircraft