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Flugmechanik
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Aerodynamic Three-Axis Attitude Stabilization of a Spacecraft by Center-of-Mass Shifting
Aerodynamic Three-Axis Attitude Stabilization of a Spacecraft by Center-of-Mass Shifting
Aeroelastic Design of Blended Composite Structures Using Lamination Parameters
Aeroelastic Stability of Hingeless Rotor Blades in Hover Using Fully Intrinsic Equations
Aeroelastic tailoring of an NLF forward swept wing
Aeroservoelastic modeling and analysis of a six-DOF hypersonic flight vehicle
Aerostructural Performance of Distributed Compliance Morphing Wings: Wind Tunnel and Flight Testing
A framework of frequency-domain flight dynamics modeling for multi-rotor aerial vehicles
A Hybrid Optimal Control Approach to Fuel-Efficient Aircraft Conflict Avoidance
Aircraft directional stability and vertical tail design: A review of semi-empirical methods
Aircraft Wake-Vortex Encounter Analysis for Upper Levels
Airfoil performance degradation by coupling effects of supercooled raindrop icing and heavy rainfall
Alternative Trim Analysis Formulations for Vehicles with Redundant Multi-Axis Control Surfaces
Analysis of Stall Aerodynamics of a Swept Wing with Laminar-Flow Glove
Analysis of Strouhal number based equivalence of pitching and plunging airfoils and wake deflection
Analysis of trimmable conditions for a civil aircraft with active high-lift system
Analytical modeling of a cyclorotor in hovering state
An energy method for flutter analysis of wing using one-way fluid structure coupling
A new approach for optimum selection of a turbocharger using a genetic algorithm
A new method for design of fixed wing micro air vehicle
An improved high-lift aerodynamic prediction method for transport aircraft
Anisotropic Adaptation for Transonic Flows with Turbulent Boundary Layers
Applicability of a Counterpropagating Laser Airspeed Sensor to Aircraft Flight Regimes
Approximation of Off-Body Sonic-Boom Analysis for Low-Boom Conceptual Design
Ascent Trajectories of Hypersonic Aircraft: Operability Limits Due to Engine Unstart
Aspect-Ratio Effects on Aeromechanics of Membrane Wings at Moderate Reynolds Numbers
Assessment of Helicopter Model Accuracy Through Inverse Simulation
Assessment of Noise Level Variations of Aircraft Flyovers Using Acoustic Arrays
A two-element high-lift airfoil in disturbed flow conditions
Auralization of Flyover Noise from Open-Rotor Engines Using Model-Scale Test Data
Automatic Design of Wing–Body–Nacelle Configurations for Minimum Drag
Average Daily Radiation Dose as a Function of Altitude, Latitude, and Shielding