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Flugmechanik
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ACS3 - Flight Dynamics for A Solar Sail Technology Demonstration Mission
GPM Orbital Maintenance Planning and Operations in Low Solar Activity Environment
Flight Dynamics and Navigation Performance of the BioSentinel Mission
Interpretation of Vehicle Tumbling Predictions from 6-DOF Entry and Descent Simulation
Aeroservoelastic Modeling of Body Freedom Flutter for Control System Design
Aerodynamic Coefficients of a 70-deg Spherecone in Hypersonic Flow
Overview of Additively Manufactured TPS Proposed Flight Test and Earth Re-Entry Capsule Design
Radio Navigation of Deep Space 1 During Ion Propulsion Usage
Magnetic Suspension Wind Tunnel Reconstruction Using an Extended Kalman Filter Framework
One Giant Leap for Womankind: An Aerodynamic Study of the SLS Rocket ft. Pressure-Sensitive Paint
Method for Extracting Aerodynamic Coefficients and Winds On-the-Fly Using Real-Time GPS Data
Influence of Length-Scale Correction on Predicting Aeronautical Flows
Ongoing Aeroelastic Prediction and Validation Activities at NASA Langley Research Center
Optimizing Proprotor Blades Using Coupled Aeroacoustic and Aerodynamic Sensitivities
Investigation of Aerodynamic Matching Sensitivities for Conceptual Design
Wind Tunnel Testing of Static Aerodynamic and Power Consumption Characteristics of an Octocopter
Rotorcraft Flight Dynamics and Controls Research at NASA
The NASA Juncture Flow Test as a Model for Effective CFD/Experimental Collaboration
Aerodynamic Implications of Aerocapture Systems for Uranus Orbiters
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
Transonic Drag Reduction Through Trailing-Edge Blowing on the FAST-MAC Circulation Control Model
Overview of Low-Speed Aerodynamic Tests on a 5.75% Scale Blended-Wing-Body Twin Jet Configuration
Mechanisms of Active Aerodynamic Load Reduction on a Rotorcraft Fuselage With Rotor Effects
Status of Computational Aerodynamic Modeling Tools for Aircraft Loss-of-Control
Experimental Investigation of Rotorcraft Outwash in Ground Effect
High Altitude Venus Operations Concept Trajectory Design, Modeling and Simulation
Experiment Design for Complex VTOL Aircraft with Distributed Propulsion and Tilt Wing
High-Fidelity Aerodynamic Analysis and Optimization of the SUSAN Electrofan Concept