COMPARISON OF HOTSHOT TUNNEL FORCE, PRESSURE HEAT-TRANSFER AND SHOCK SHAPE DATA WITH SHOCK TUNNEL DATA,

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. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1964
Accession Number
AD0428916

Entities

People

  • E. E. Edenfield

Organizations

  • Arnold Engineering Development Complex

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Agreements
  • Buildings And Structures
  • Energy Transfer
  • Heat Transfer
  • Observatories
  • Research Facilities
  • Shock Tunnels
  • Test Facilities

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.