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Flugmechanik
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keywords:("Flugmechanik")
Influence of rotor wakes on helicopter aerodynamic behaviour
Flight Dynamics Aspects of a Large Civil Tiltrotor Simulation Using Translational Rate Command
Modeling Powered Aerodynamics for the Orion Launch Abort Vehicle Aerodynamic Database
Aerodynamic Characterisation of an Experimental Tilt-Wing Aircraft
Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints
Blade Displacement Measurements of the Full-Scale UH-60A Airloads Rotor
Recent Developments at the NASA Langley Research Center National Transonic Facility
System Identification Applied to Dynamic CFD Simulation and Wind Tunnel Data
Aerodynamic Testing of the Orion Launch Abort Tower Separation with Jettison Motor Jet Interactions
ARES I Aerodynamic Testing at the NASA Langley Unitary Plan Wind Tunnel
Numerical Investigation of Rotorcraft Fuselage Drag Reduction Using Active Flow Control
Deep-Space Conjunction Assessment: Recent Developments and Future Evolution
Rapid Automated Aircraft Simulation Model Updating from Flight Data
Correlating CFD Simulation with Wind Tunnel Test for the Full-Scale UH-60A Airloads Rotor
Dragonfly Entry and Descent Flight Mechanics Modeling and Analysis for Mission PDR
Experimental Investigation of a Large-Scale Low-Boom Inlet Concept
Reynolds-Averaged Navier-Stokes Simulation of a 2D Circulation Control Wind Tunnel Experiment
Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel
Improved Aerodynamic Analysis for Hybrid Wing Body Conceptual Design Optimization
High-Fidelity Analysis of Six-Passenger Quadrotor Air Taxi Concept
An Assessment of Flap and Main Landing Gear Noise Abatement Concepts
Active Flow Control of Lifting Surface With Flap-Current Activities and Future Directions
Engine Yaw Augmentation for Hybrid-Wing-Body Aircraft via Optimal Control Allocation Techniques
Development of EC 135 turbulence models via system identification
A New Aerodynamic Data Dispersion Method for Launch Vehicle Design
Flow Control on Low-Pressure Turbine Airfoils Using Vortex Generator Jets
NASA High-Reynolds Number Circulation Control Research - Overview of CFD and Planned Experiments
Shock Tube and Ballistic Range Facilities at NASA Ames Research Center
Overview of the Novel Intelligent JAXA Active Rotor Program
Characterization of the Effect of Wing Surface Instrumentation on UAV Airfoil Performance
Basis Function Approximation of Transonic Aerodynamic Influence Coefficient Matrix
An Interactive Preliminary Design System of High Speed Forebody and Inlet Flows
Conceptual Feasibility Study of the Hyperloop Vehicle for Next-Generation Transport
2-D Circulation Control Airfoil Benchmark Experiments Intended for CFD Code Validation
Aerodynamic Design of a Part-Span Tandem Bladed Rotor for Low Speed Axial Compressor