Hypersonic dynamic stability.

pt. 1. Summary [by] L. A. Marshall.--pt. 2. Conical body experimental program [by] R. B. Hobbs, Jr.--pt. 3. Unsteady flow field program [by] H. Rie, E. A. Linkiewicz [and] F. D. Bosworth.

Hypersonic free flight research.

pt. 1 Instrumentation evaluation and data analysis, by R. W. Bogle and R. J. Magnus.--pt. 2 Investigations of heat trasfer and aerodynamic stability, by O. R. Burggraf.

Investigation of feasibility of utilizing available heat resistant materials for hypersonic leading edge applications.

"Volumes I through VIII are unclassified while volume IX is classified secret."

Recent advances in structures for hypersonic flight : proceedings of a symposium held at Langley Research Center, Hampton, Virginia, September 6-8, 1978.

Includes bibliographical references.

Hypersonic gas dynamic charts for equilibrium air /

Errata sheet inserted.

Approximate solutions for nonequilibrium airflow in hypersonic nozzles,

Contract no. AF40(600)-804. AEDC TN-60-181. Arnold Engineering Development Center, Arnold Air Force Station, Tennessee. Air Research and Development Command, United States Air Force."

A study of the overall problems of the true-temperature, hypersonic wind tunnel having semi-continuous operation and the preferred methods of solution.

"Supported by the McDonnell Aircraft Corporation under Contract no. 6140-20 P. O. 7S4899-R. Purdue Research Foundation. Research project no. 1717. Project Ae-33.

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

Recent developments connected with the hypersonic facility of the Polytechnic Institute of Brooklyn. Pt. I: Tests of the compression heater. Pt. II: Aspects of the design, construction and installation of a multiple-outlet collector for the convection heater.

Mode of access: Internet.

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."

Nonequilibrium scaling criterion for inviscid hypersonic airflows,

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