Accession Number:

AD0851657

Title:

Heat Transfer Rate Distribution on Azusa Antenna Strut,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s):

Report Date:

1960-06-15

Pagination or Media Count:

9.0

Abstract:

A scale model of the Azusa antenna was tested to determine the effects of the antenna fairing on the heat transfer rate distribution on the strut. The tests were conducted at Mach 6.6 and a total gas temperature of 4000 degrees R in the Thermodynamics Laboratories rocket-powered wind tunnel. Author

Subject Categories:

  • Structural Engineering and Building Technology
  • Surface-Launched Guided Missiles
  • Thermodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE