A study of finite-difference methods as applied to hypersonic viscous shock-layer equations

"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)."

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."

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.

Validity of air data equations at high altitudes.

Mode of access: Internet.

Research on rotating stall in axial flow compressors.

"January 1959."

Roll-yaw control at high angle of attack by forebody tangential blowing /

"October 1995."

Application of the pressure sensitive paint technique to steady and unsteady flow /

"June 1996."

Wind tunnel tests of thin airfoils oscillating near stall.

"January 1969."

NACA conference on some problems of aircraft operation; a compilation of the papers presented.

"Papers presented ... on October 9 and 10, 1950."

Demand bibliography : computational fluid dynamics /

"Sample."