IMPACT OF A SUPERSONIC JET AGAINST A SURFACE,

Abstract

The shape and location of the shock wave and the value of the mean parameters of subsonic gas movement between the shock wave and the surface are determined on the basis of some approximations. The gas is assumed to be ideal and calorically perfect. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 10, 1967
Accession Number
AD0663078

Entities

People

  • A. Ya. Sagomonyan

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

DTIC Thesaurus Topics

  • Shock
  • Shock Waves
  • Waves

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Fluid Dynamics.

Technology Areas

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