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Flugmechanik
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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
Ongoing Subsonic Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch
AeroFusion: Data Fusion and Uncertainty Quantification for Entry Vehicles
Hydrocarbon Cold-Flow Simulation of LOX/LH2 Rocket Aerodynamics
Ongoing Aeroelastic Prediction and Validation Activities at NASA Langley Research Center
Aerodynamic Implications of Aerocapture Systems for Uranus Orbiters
FUN3D Airload Predictions for the Full-Scale UH-60A Airloads Rotor in a Wind Tunnel
Thermal Snap of Satellite Solar Panels
Application of the CATNLF Design Method to a Transonic Transport Empennage Using CDISC
Investigation on rotor blade-wake interaction noise in descent flight conditions
Rotorcraft Flight Dynamics and Controls Research at NASA
In search of data-driven improvements to RANS models applied to separated flows
Ablating Woven Thermal Protection System Materials Under High Shear Flow Conditions
Ongoing Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch
Inside NASA’s X-57 Configuration - More than Just Electrifying an Airplane
Propulsive trajectory optimization to minimize surface contamination
Radio Navigation of Deep Space 1 During Ion Propulsion Usage
Ongoing Subsonic Aeroelastic Optimization Research at NASA LaRC, Aeroelasticity Branch
Development of Aerodynamic Loads Databases for the Space Launch System Booster Separation Event
NASA Armstrong Flight Research Center Dynamics and Controls Branch
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
Air-bearing facility for the simulation of spin-stabilized satellites
Hypersonic Vehicles : Past, Present and Future Developments
Hypersonic Vehicles : Past, Present and Future Developments
Adjoint-Based Mesh Adaptation and Shape Optimization for Simulations with Propulsion
Nonlinear Fuzzy Hybrid Control of Spacecraft
The Rise of Unstructured-Grid Methodology In Modern Aerodynamic Analysis and Design
Aerodynamic Implications of Aerocapture Systems for Uranus Orbiters
Prandtl Propeller Project: Understanding, Researching and Designing Propellers