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Comparison of Hotshot Tunnel Force, Pressure, Heat-Transfer and Shock Shape Data with Shock Tunnel Data

Report Number: AEDC TDR 64-1
Author(s): E. E. Edenfield
Corporate Author: ARO, Inc.
Date of Publication: 1964-01
Pages: 25
Contract: AF 40(600)-1000
Project: None Given
AD Number: AD0428916

Abstract:
Comparison is made of force, pressure, heattransfer, 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.

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