Wave superheater hypersonic tunnel; semiannual report,

"AEDC TDR-62-54. Program area 750A. AFSC project 4773. Contract no. AF40(600)-804."

The turbulent boundary layer with variable Prandtl number.

Mode of access: Internet.

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.

Airplane design; a textbook of airplane layout and stress analysis calculations with particular emphasis on economics of design.

"First three editions comprising 2400 copies were published between Dec. 1934 and June 1939."

Recirculation principle for ground effect machine two-dimensional tests.

"Task 9R99-01-005-04. Contract DA 44-177-TC-710."

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

"Contract no. Nonr 2653(00)"

Engineering design of a wave superheater facility for hypersonic research and development.

AFOSR-TN-59-108; AD-210224.

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)."

Hypersonic research summary.

"Contract AF 18(603)-141. Mechanics Division, Air Force Office of Scientific Research, Air Research and Development Command, Washington."

Low-density research in the hypersonic shock tunnel

"The experimental study reported here has been performed under the sponsorship of the Fluid Dynamics Branch, Aeronautical Research laboratories of the U.S. Air Force Air Research and Development Command, Contract no. AF 33(616)-6025."

Expansion of gas clouds and hypersonic jets bounded by a vacuum.

"SSD-TDR-62-96. Report no. TDR-169 (3230-12) TR-1. Contract no. AF 04(695)-169."

Extended hypervelocity gas dynamic charts for equilibrium air.

"Prepared for the Air Force Ballistic Missile Division, Headquarters Air Research and Development Command, under Contract AF (04(647)-309, Magnetoaerodynamic Research."

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."

48-inch hypersonic shock tunnel; description and capabilities.

Mode of access: Internet.

Six-degree-of-freedom equations of motion for a maneuvering re-entry vehicle

Cover title.