Jim A Penland
Aerodynamic characteristics of a hypersonic research airplane concept having a 70ê swept double-delta wing at Mach number 0.2- Aerodynamic characteristics of a hypersonic research airplane concept having a 70ê swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0
- Low-speed aerodynamic characteristics of a lifting-body hypersonic research aircraft configuration
- Wall-temperature effects on the aerodynamics of a hydrogen-fueled transport concept in Mach 8 blowdown and shock tunnels