VIBRATIONS OF A SUPERSONIC GAS FLOWING IN A FINITE CHANNEL WITH OSCILLATING WALLS,

Abstract

The purpose of the study is to determine the pressure on the walls of a cylindrical channel taking account of the influence of the waves reflected from the axis.

Document Details

Document Type
Technical Report
Publication Date
Mar 21, 1966
Accession Number
AD0644175

Entities

People

  • D. A. Derbentsev

Organizations

  • Lockheed Martin Missiles and Space

Tags

DTIC Thesaurus Topics

  • Mechanical Waves
  • Vibration
  • Waves

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

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