A H Boudreau

发表

Pressure and Heat Transfer Tests on the NASA Space Shuttle External Tank at Mach Number 16

L G Siler, A H Boudreau, 1975 .

Artificially Induced Transition Results from a 7-Deg, 14-7-Deg Biconic, and 5-Deg Cone at Mach 9 in the AEDC-VKF Tunnel F

A H Boudreau, 1978 .

Artificially Induced Boundary-Layer Transition on Blunt-Slender Cones Using Distributed Roughness and Spherical-Type Tripping Devices at Hypersonic Speeds

A H Boudreau, A. Boudreau, 1978 .

Performance and Operational Characteristics of AEDC/VKF Tunnels A, B, and C

A H Boudreau, 1981 .

Transition Measurements via Heat-Transfer Instrumentation on a 0.5 Bluntness 9.75-deg Cone at Mach 7 with and without Mass Addition

A H Boudreau, 1985 .