USAF damage tolerant design handbook : guidelines for the analysis and design of damage tolerant aircraft structures : final report for period September 1980 to March 1984 /

"May 1984."

A 50-megawatt arc heater: scaling parameters and performance prediction

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

Skin friction, heat transfer, and pressure measurements on hypersonic inlet compression surfaces in the Mach number range 7.5 to 16.

Cornell Aeronautical Laboratory, Inc., Buffalo. Report no. AA-1948-Y-3

Research on developing design criteria for anti-friction airframe bearings for high temperature use.

"This report was prepared by the Research and Development Department of the New Departure Division, General Motors Corporation in Bristol, Connecticut."

Development of a continuous flow electromagnetic alternating current traveling wave accelerator for high-density, hypervelocity wind tunnel applications,

Mode of access: Internet.

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."

Performance improvement of arc heaters for aerodynamic wind tunnels

Mode of access: Internet.

Experimental studies of high temperature hypersonic diffusers.

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

Axisymmetric Hall-arc jet wind tunnel driver study

Mode of access: Internet.

Analysis of several handling quality topics pertinent to advance manned aircraft.

Mode of access: Internet.

Computer program for one-dimensional nonequilibrium reacting gas flow

Mode of access: Internet.

Optimum shape for transpiration-cooled nosetip of a re-entry vehicle /

"Technical report AFFDL-TR-78-147. Final report for period October 1974-June 1978."

M=3 turbulent boundary layer measurements at very high Reynolds numbers /

"Interim report for period January 1975 to September 1976."

Experimental modal analysis and dynamic component synthesis

Mode of access: Internet.

Similitude for normal shock waves in nonequilibrium flows

Mode of access: Internet.