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