Charles B Johnson

• A description of the active and passive sidewall-boundary-layer removal systems of the 0.3-Meter Transonic Cryogenic Tunnel
• Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6
• Heat-transfer and pressure measurements on a simulated elevon deflected 30 ̊near flight conditions at Mach 7
• Heat-transfer and pressure measurements on a simulated elevon deflected 30ê near flight conditions at Mach 7
• Theoretical study of nonadiabatic boundary-layer stabilization times in a cryogenic wind tunnel for typical stainless-steel wing and fuselage models