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Flugmechanik
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Hypersonic Vehicle Flight Dynamics with Coupled Aerodynamic and Reduced-Order Propulsive Models
Flight Mechanics of a Tailless Articulated Wing Aircraft
Nonlinear Aircraft Model Identification and Validation for a Fault-Tolerant Flight Control System
Joined Wings Thrust Vectored UAV Flight Envelope
ACS3 - Flight Dynamics for A Solar Sail Technology Demonstration Mission
L~1 Adaptive Control of Flexible Aircraft: Preliminary Results
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
Wind-Shear Endurance Capability for Powered-Lift Aircraft
Simulated Rarefield Aerodynamics of the Magellan Spacecraft During Aerobraking
Wind-Tunnel Investigation of Wind-Shear Effect on Turning Flight
Minimum-Fuel Trajectories for Hypersonic Vehicles with Aeropropulsive Interactions
A New Flying Qualities Criterion for Flying Wings
Effect of Rotary Atmospheric Gusts on Fighter Airplane
Aerodynamic Coefficients of a 70-deg Spherecone in Hypersonic Flow
Overview of Additively Manufactured TPS Proposed Flight Test and Earth Re-Entry Capsule Design
Agricultural Tractor Tire Dynamic Indices
Aircraft with Single Axis Aerodynamically Deployed Wings
A Method of Wind Shear Detection for Powered-Lift STOL Aircraft
Radio Navigation of Deep Space 1 During Ion Propulsion Usage
Method for Extracting Aerodynamic Coefficients and Winds On-the-Fly Using Real-Time GPS Data
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
Influence of Length-Scale Correction on Predicting Aeronautical Flows
Mission Performance Measures for Spacecraft Formation Flying
Ongoing Aeroelastic Prediction and Validation Activities at NASA Langley Research Center
Nonlinear Fuzzy Hybrid Control of Spacecraft
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
An Automated Real-Time Spacecraft Navigation System
Rotorcraft Flight Dynamics and Controls Research at NASA
The NASA Juncture Flow Test as a Model for Effective CFD/Experimental Collaboration