PRESSURE DISTRIBUTION IN THE WAKE OF TWO BODIES OF REVOLUTION AT TRANSONIC AND SUPERSONIC SPEEDS,

Abstract

An experimental investigation of the wake of two bodies of revolution at transonic and supersonic speeds has been conducted. Static pressure and Mach number distribution along the wake centerline and total pressure profiles across the wake are presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1963
Accession Number
AD0427748

Entities

People

  • Helmut G. Heinrich
  • R. Sheldon Hess

Organizations

  • University of Minnesota

Tags

DTIC Thesaurus Topics

  • Bodies
  • Bodies Of Revolution
  • Mach Number
  • Pressure Distribution
  • Revolutions
  • Static Pressure

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow