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Aerodynamik
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Integrated Numerical and Experimental Workflow for High-Performance Vehicle Aerodynamics
6 degrees of freedom simulation of an unguided sounding rocket using Matlab/Simulink
Uncertainty Analysis of Store Separation Aerodynamic Data at the NRC 1.5 M Trisonic Wind Tunnel
Integration of Arc-Jet in Impulse Facility for Hypervelocity Aerothermal Testing with Ablation
Electromagnetic Modeling of Wind Tunnel Magnetic Suspension and Balance Systems
A Propeller Test Stand for Testing in the NASA Langley Low Speed Aeroacoustic Wind Tunnel
Spectroscopic Characterization of a High-Enthalpy Plasma Arcjet Tunnel
Advanced Optical Diagnostics in an Axis-Symmetric Mach 5 Glass Blown Nozzle
Effects of Separation Region Reattachment on the Dynamic Motion of Low-Fineness Ratio Cylinders
LAVA CFD Analysis of the Check Standard Model Within the Langley Unitary Plan Wind Tunnel
NASA’s Unsteady Pressure-Sensitive Paint Research and Operational Capability Developments