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Flugmechanik
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Influence of Mass Parameters Modification on Manoeuvrability of 9K33 „OSA” Set 9M33M3 Missile
Air Traffic Management and Control
Air Traffic Management and Control
Air Traffic Management and Control
Aeroelastic Analysis of Highly Flexible Wings with Linearized Frequency-Domain Aerodynamics
Nonlinear Fuzzy Hybrid Control of Spacecraft
Free-Fight Dynamics of an Aeroshell/Drogue Parachute System
The Rise of Unstructured-Grid Methodology In Modern Aerodynamic Analysis and Design
Aerodynamic Implications of Aerocapture Systems for Uranus Orbiters
Hypersonic Vehicles : Past, Present and Future Developments
Hypersonic Vehicles : Past, Present and Future Developments
NASA Armstrong Flight Research Center Dynamics and Controls Branch
Design of a Slotted, Natural-Laminar-Flow Airfoil for a Transport Aircraft
Prandtl Propeller Project: Understanding, Researching and Designing Propellers
Optimizing Proprotor Blades Using Coupled Aeroacoustic and Aerodynamic Sensitivities
Investigation of Aerodynamic Matching Sensitivities for Conceptual Design
Concept Design of a 5 MW Partially Superconducting Generator
Effects of 3D Roughness Patch on Transition in High-Speed Boundary Layers
Wind Tunnel Testing of Static Aerodynamic and Power Consumption Characteristics of an Octocopter
Status of Data-Driven Improvements to the Spalart-Allmaras Model Applied to Multiple Configurations
Dragonfly Entry and Descent Flight Mechanics Modeling and Analysis
Adjoint-Based Mesh Adaptation and Shape Optimization for Simulations with Propulsion
Flight Dynamics Research Facility - Perspective on Future Impacts
Aerodynamics and Performance Flight Research and Airworthiness Best Practices
Rotorcraft Flight Dynamics and Controls Research at NASA
Propulsive trajectory optimization to minimize surface contamination
The NASA Juncture Flow Test as a Model for Effective CFD/Experimental Collaboration
An Automated Real-Time Spacecraft Navigation System
Flight mechanical analysis of a solar-powered high-altitude platform
Free Flight Ground Testing of ADEPT in Advance of the Sounding Rocket One Flight Experiment
Aerial Robots : Aerodynamics, Control and Applications
Aerial Robots : Aerodynamics, Control and Applications
Integrated Software Architecture for Solar Cruiser Mission Design and Navigation
A Method of Ground Resonance Testing for Helicopters
Mid-Lift-To-Drag Ratio Rigid Vehicle 6-DOF EDL Performance Using Tunable Apollo Powered Guidance
Mid-Lift-to-Drag Ratio Rigid Vehicle 6-DOF EDL Performance Using Tunable Apollo Powered Guidance