Parametric Inlet Tested in Glenn's 10- by 10-Foot Supersonic Wind Tunnel
Shock-Tunnel Combustor Testing for Hypersonic Vehicles
Aerodynamic Investigation of Incidence Angle Effects in a Large Scale Transonic Turbine Cascade
Lessons Learned During TBCC Design for the NASA-AFRL Joint System Study
Assessment of Aerodynamic Performance of V/STOL and STOVL Fighter Aircraft
Effects of Inlet Spillage on Store Carriage Loads and Launch Trajectories
NASA (National Aeronautics and Space Administration) Supersonic STOVL Propulsion Technology Program
High Total Temperature Sensing Probe for the X-15 Hypersonic Aircraft