Parametric Inlet Tested in Glenn's 10- by 10-Foot Supersonic Wind Tunnel
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
NASA (National Aeronautics and Space Administration) Supersonic STOVL Propulsion Technology Program
High Total Temperature Sensing Probe for the X-15 Hypersonic Aircraft
Effects of Inlet Spillage on Store Carriage Loads and Launch Trajectories