Special Properties of Supersonic Gas Flows in Perforated Boundaries,

Abstract

The development history, operating principles, and potentialities of supersonic nozzles with perforated edges are briefly discussed. It is pointed out that the properties of supersonic flows in perforated boundaries can be used in many regions of technology. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 05, 1973
Accession Number
AD0754601

Entities

People

  • G. L. Grodzovakii

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Flow
  • Gas Flow
  • Supersonic Flow
  • Supersonic Nozzles

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight