Comparison of hotshot tunnel force, pressure heat-transfer and shock shape data with shock tunnel data /
by E.E. Edenfield.

Description

Main Author

Edenfield, E. E.

Related Names

ARO, Inc.
Arnold Engineering Development Center
United States. Air Force.

Language(s)

English

Published

Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964.

Subjects

Hypersonic wind tunnels.
Cone > Cone / Aerodynamics.
Shock tunnels.

Summary

Comparison is made of force, pressure, heat-transfer, and shock shape data from tests in the AEDC-VKF hotshot tunnels and in the Cornell Aeronautical Laboratory 48 Inch Shock Tunnel. Several cone models of varying bluntness were tested through an angle-of-attack range of 0 to 40 deg at each facility. Excellent agreement of the hotshot and the shock tunnel data is shown. (Author).

Note

"January 1964."

Physical Description

25 pages : illustrations, 28 cm

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