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Aerodynamik
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keywords:("Aerodynamik")
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
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
Renewed Characterization of a Mach 6 Hypersonic Wind Tunnel
LAVA CFD Analysis of the Check Standard Model Within the Langley Unitary Plan Wind Tunnel
Scramjet Inflow Characterization Based on Thermodynamic Analysis of Arc-Heater Plenum
Infrared Reflection Removal in Wind Tunnels Using Polarization Theory
Design and Development of an Aircraft Electric Powertrain Test Stand
Laser-Based In-situ Absorption Spectroscopy Sensor for Gas Measurements in an Impulse Facility
NASA’s Unsteady Pressure-Sensitive Paint Research and Operational Capability Developments