Kinetic study of the hypersonic flow past the leading edge of a flat plate.

Vita.

An analytical and experimental study of the ionized flow field about a hemisphere cylinder and its effect on the radiation pattern of a slot antenna

Mode of access: Internet.

The blunt-body problem in hypersonic flow at low Reynolds number.

"Contract no. Nonr 2653(00)"

Hypersonic flow with combined leading-edge bluntness and boundary-layer displacement effect.

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

Experiments in transonic flow,

"Prepared by the California Institute of Technology, Pasadena, California, in June 1947, under AAF contract no. W33-038 ac-1717 (11592), supplemental agreement no. 6."

Research on rotating stall in axial flow compressors.

"January 1959."

Basic studies of rotating stall and an investigation of flow-instability sensing devices

pt. 1. Basic studies of rotating stall flow mechanisms.--pt. 2. Investigation of flow-instability sensing devices.

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."

Effects of ambient nonuniformities in flow over hypersonic test bodies.

Mode of access: Internet.

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.

An analysis of nonequilibrium inviscid flow,

"Air Force contract no. AF40(600)-928."

Linearized theory of conical supersonic flow with application to triangular wings /

Loose-leaf.

On the use of impact theory for slender configurations exhibiting flow separation /

Photocopy.

Nonsteady discharge of subcritical flow /

At head of title: Project SQUID, a cooperative program of fundamental research as related to jet propulsion, Office of Naval Research, Department of the Navy. Contract Nonr 1858 (25), NR-098-038.

A new method for providing continuous high-temperature air flow for hypersonic research,

"AFOSR-TN-56-236."