The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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

Report Number: AEDC TDR 64-1
Author: 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

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.

This report has yet to be scanned by Contrails staff

Request scanning of this report

Other options for obtaining this report

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a full-image download of the report, exists at DTIC

Via National Technical Information Service:
This report may have been digitized and made freely available for public download, or made publicly available for purchase by the National Technical Information Service through their online database, the National Technical Reports Library

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
There has been no verification of an indication of public availability from an inside cover statement