Graduate Student Support in Supersonic Diagnostics and Flow, (FY91 AASERT).

Abstract

This project is directed toward obtaining a more fundamental understanding of mixing and chemical reaction in supersonic flows. The research effort comprises three inter-related elements: (1) an experimental study of mixing and combustion in a supersonic plane mixing layer; (2) development of laser-based diagnostics for high-speed flows; and, (3) simulations of compressible reacting flows. (MM)

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Document Details

Document Type
Technical Report
Publication Date
Jul 14, 1995
Accession Number
ADA297936

Entities

People

  • Craig T. Bowman

Organizations

  • Stanford University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Chemical Reactions
  • Combustion
  • Endothermic Reactions
  • Exothermic Reactions
  • Flow
  • Simulations
  • Supersonic Aircraft
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Combustion Dynamics and Shock Wave Physics.
  • Computational Fluid Dynamics (CFD)
  • Research Science/Academic Research

Technology Areas

  • Directed Energy
  • Hypersonics