Heat Transfer Rate Distribution on Azusa Antenna Strut,

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)

Document Details

Document Type
Technical Report
Publication Date
Jun 15, 1960
Accession Number
AD0851657

Entities

People

  • F. P. Baltakis

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Buildings And Structures
  • Energy
  • Energy Transfer
  • Heat Energy
  • Heat Transfer
  • Research Facilities
  • Scale Models
  • Thermodynamics
  • Wind Tunnels

Readers

  • Aerodynamics.
  • Positioning, Navigation, and Timing (PNT) Technology.
  • Rocket Propulsion.