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Flugmechanik
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Study of Missile Aerodynamic Characteristics in the Process of Crossing the Carrier's Shock Wave
Multiple Roll Angle Fitting of Static Aerodynamic Coefficients of Cruciform Missiles
Comparison of Conventional and Asymmetric Aircraft Configurations Using CEASIOM
Simulation of Aircraft Manoeuvres Based on Computational Fluid Dynamics
Stability of an Unmanned Airplane Using a Low-Order Panel Method
A Multidimensional Spline-Based Global Nonlinear Aerodynamic Model for the Cessna Citation II
Control Law Design for Perching an Agile MAV with Articulated Wings
The Hypersonic Dynamic Characteristics of Waverider
Hypersonic Stability Derivative Modeling Issues
Flight Dynamics Properties of 155 mm Spin-Stabilized Projectiles Analyzed in Different Body Frames
Control of a Stochastic Model of an Aeroelastic Micro Air Vehicle in Turbulence (AIAA 2013-4983)
Effects of Periodic Flight Trajectory on Endurance of a Remotely Piloted Aircraft (AIAA 2013-5163)
Flight Stability and Control of Articulated Wing Aircraft (AIAA 2013-4982)
Parameter Identification Technique based on Lyapunov Stability (AIAA 2013-4750)
Trajectory Control of Very Flexible Aircraft with Gust Disturbance (AIAA 2013-4745)
Flight Performance Feasibility Studies for the Max Launch Abort System (AIAA 2013-4685)
Nano-Satellite Deorbit by Bare Electrodynamic Tether (AIAA 2013-4683)
Statistical Impact Prediction of Decaying Objects (AIAA 2013-4682)
Towards the Design of a Pilot-induced-oscillation Detection and Mitigation Scheme (AIAA 2013-4605)
Time-Accurate Computations for Rapid Generation of Missile Aerodynamics
Virtual Aircraft Design and Control of TransCruiser - A Canard Configuration
A Wake-Only Energetics Model for Preliminary Design of Biologically Inspired Micro Air Vehicles
Nonlinear Aircraft Model Identification and Validation for a Fault-Tolerant Flight Control System
Experimental Study of Gust Effects on Micro Air Vehicles
Tethered Aerostat Modeling Using an Efficient Recursive Rigid Body Dynamics Approach
A UAV Model Parameter Identification Method
Some Applications of a Panel Method to Aerodynamic Modeling of Missiles
System Identification of an Ornithopter Aerodynamics Model
Flight Tests, Performances and Flight Certification of a Twin-Engine Light Aircraft
Joined Wings Thrust Vectored UAV Flight Envelope
Aeroelastic Modeling and Adaptive Control of GTM
Aerodynamic Optimization for Subsonic Fixed Wing UAV (AIAA 2013-5089)
Spin Susceptibility of the NASA Generic Transport Model (AIAA 2013-5081)
Rotorcraft Slope Landings with Articulated Landing Gear (AIAA 2013-5160)
Handling Qualities Evaluation of a VMCG Reduction Functionality (AIAA 2013-4504)
Stability Analysis in Conceptual Design Using SDSA Tool
Modeling of Dynamic Loading of Morphing Wing Aircraft
Aerodynamic and Structural Measurement of the Aerostructures Test Wing for Flutter Testing
Effects of Wing Design on Aerodynamics of MAVs in Turbulent Flow
Flight Mechanics of a Tailless Articulated Wing Aircraft