Stability of the boundary layer;

Reproduced from typewritten copy.

Vector polar method for shock interactions with area disturbances /

"AFOSR TN 59-701. Contract no. AF49(638)-166. I. E. R. project no. 96895."

Pressure gradient effects on supersonic boundary layer turbulence : final report /

"Carried out by the Fluid Mechanics Section of the Aeronutronic Division of the Ford Aerospace & Communications Corporation."

Boundary layer and wake modifications to compressor design systems : the effect of blade-to-blade flow variations on the mean flow field of a transonic rotor : final report, 01 September 1976-31 August 1978 /

"AFAPL-TR-79-2010."

The shock layer concept and three-dimensional hypersonic boundary layers.

"This report is based on research sponsored by the U.S. Navy through the Office of Naval Research, Contract Nonr-2653(00)"

Effects of ambient nonuniformities in flow over hypersonic test bodies.

Mode of access: Internet.

Instrumentation for force and pressure measurements in a hypersonic shock tunnel

Mode of access: Internet.

Radiation at hypersonic speeds.

Mode of access: Internet.

Hypersonic research in the shock tunnel.

"Presented at the I.A.S. National Symposium on Hypervelocity Techniques, Denver, Colorado, October 20, 21, 1960."

Theoretical and experimental studies of airfoil characteristics in nonuniform sheared flow.

At head of title: Task 1P125901A142. Contract DA 44-177-AMC-70 (T). USAAML technical report 65-17.

Nonequilibrium scaling criterion for inviscid hypersonic airflows,

"Contract no. DA-30-069-ORD-3443. ARPA order no. 253-62."

A similitude for nonequilibrium phenomena in hypersonic flight,

"Part I of the present paper was supported by the Arnold Engineering Development Center under Contract no. AF-40-(601)-928. Part II is a part of project DEFENDER sponsored by the Advanced Research Projects Agency, Department of Defense, under Contract no. DA-30-069-ORD-3443."

An investigation of laminar heat transfer to slender cones in the hypersonic shock tunnel

"Contract no. AF-33(616)-6025. Project no. 7064. Task no. 70169. Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, Wright-Patterson Air Force Base."

Shock tunnel studies of high-enthalpy ionized airflows,

"AFOSR 3025."

Experimental studies of high temperature hypersonic diffusers.

"Project No. 1426. Task No. 142612."