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
A Propeller Test Stand for Testing in the NASA Langley Low Speed Aeroacoustic Wind Tunnel
Electromagnetic Modeling of Wind Tunnel Magnetic Suspension and Balance Systems
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