The Ames 10- by 14-Inch Supersonic Wind Tunnel
Description:
"The purpose of the present report is to describe the 10- by 14-inch supersonic wind tunnel and its operational characteristics over the nominal Mach number range from 2.7 to 6.3. Rather complete calibration data on characteristics of flow in the test section are presented and briefly discussed" (p. 2).
Date:
January 1954
Creator:
Eggers, A. J., Jr. & Nothwang, George J.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department