DETERMINATION OF UPWASH AROUND A BODY OF REVOLUTION AT SUPERSONIC VELOCITIES

Abstract

The method of analysis presented is a straightforward application of the formulas for the potential flow around bodies of revolutions at supersonic velocities which have been established by H. S. Tsien (Journal of the Aeronautical Sciences, October 1938: Supersonic flow over an inclined body of revolution).

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Document Details

Document Type
Technical Report
Publication Date
May 27, 1946
Accession Number
AD0623168

Entities

People

  • L. Beskin

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Bodies
  • Bodies Of Revolution
  • Coefficients
  • Cross Flow
  • Downwash
  • Flow
  • Fuselages
  • Incompressible Flow
  • Mach Number
  • Physics Laboratories
  • Potential Flow
  • Revolutions
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Academic Conference Management
  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics