Influence of Variation of Aspect Ratio on the Pressure Recovery in Super Sonic Diffusers

Abstract

A systematic investigation was made of the gasdynamics of supersonic diffusers, in particular, diffusers applicable to gasdynamic or other types of flow lasers. The main conclusion was that almost all the research on supersonic diffusers was performed with specific application, namely a specific wind tunnel installation or an engine, in mind. Systematic studies on the gasdynamics of diffusers even of simple geometries were scarce, making it difficult, if not impossible, to extend existing work to other configurations. Despite the fact that some of the high Mach number wind tunnels operated with known unequilibrated internal modes, there was no research on nonequilibrium flow effects in diffusers in the literature consulted. Moreover, in most conventional wind tunnels, the cross-section of the test section is either circular or squarish. Consequently, most diffuser studies were concerned with circular, square, or rectangular cross-sections with comparable widths and heights, characterized by an aspect ratio, defined as the width to height ratio, of unity or close to unity.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1979
Accession Number
ADA214848

Entities

People

  • Benjamin J. Wu

Organizations

  • Yale University

Tags

DTIC Thesaurus Topics

  • Aspect Ratio
  • Boundaries
  • Boundary Layer
  • Diffusers
  • Engineering
  • Flow
  • Flow Visualization
  • Geometry
  • Laser Applications
  • Lasers
  • Mach Number
  • Nonequilibrium Flow
  • Ordnance Laboratories
  • Supersonic Diffusers
  • Supersonic Flow
  • Tubes
  • Wind Tunnels

Fields of Study

  • Engineering
  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Theoretical Analysis.

Technology Areas

  • Directed Energy
  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow