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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
A Propeller Test Stand for Testing in the NASA Langley Low Speed Aeroacoustic Wind Tunnel
NASA’s Unsteady Pressure-Sensitive Paint Research and Operational Capability Developments
Development of kHz-Rate CO Laser-Induced Fluorescence in High Speed Flows
Using Computational Fluid Dynamics for the Development of Supersonic Wind Tunnels
Testing and Characterization of the University of Tennessee High-Enthalpy Tunnel
Spectroscopic Characterization of a High-Enthalpy Plasma Arcjet Tunnel
Advanced Optical Diagnostics in an Axis-Symmetric Mach 5 Glass Blown Nozzle
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