CHANNELED BODIES STREAMLINED WITH FLAT AND CONIC SHOCK WAVES,

Abstract

Consideration is given to examples of precise solutions for external flow around channeled bodies with supersonic velocities at the inlet to the internal channel, and the corresponding coefficients are calculated. Two classes of bodies are investigated: (1) bodies consisting of flat faces and streamlined over the design regime with the formation of flat, attached shock waves, (2) axisymmetric bodies for which external flow is conic.

Document Details

Document Type
Technical Report
Publication Date
Nov 18, 1964
Accession Number
AD0609148

Entities

People

  • V. V. Keldysh

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Axisymmetric
  • Coefficients
  • Elastic Waves
  • Mechanical Waves
  • Shock
  • Shock Waves
  • Waves

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design

Technology Areas

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