DRAG CHARACTERISTICS OF PLATES, CONES, SPHERES AND HEMISPHERES IN THE WAKE OF A FOREBODY AT TRANSONIC AND SUPERSONIC SPEEDS.

Abstract

The drag coefficients of a circular flat plate, 45 degree half-angle cone, sphere and hollow hemisphere in the wake of a forebody at transonic and supersonic speeds have been calculated from the drag of a two body system. In addition, a number of direct measurements were made as a supplement to the calculated values. The investigation was carried out at Mach numbers between 0.85 and 1.25 and at M 4.35. Body size and position in the wake were the selected parameters. The drag in the wake was less than in the free stream in all but a few cases in the transonic range, where it was about equal to the free stream drag. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1964
Accession Number
AD0457056

Entities

People

  • Helmut G. Heinrich
  • Sheldon R. Hess

Organizations

  • University of Minnesota

Tags

DTIC Thesaurus Topics

  • Bodies
  • Coefficients
  • Free Stream
  • Hemispheres
  • Mach Number
  • Measurement
  • Parachutes

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow