The Structure and Control of Three-Dimensional Shock Wave Turbulent Boundary Layer Interactions.

Abstract

A review of the work completed during the first year of research on the subject contract is presented. Papers and publications generated, staff, and students involved in research are noted, along with a brief description of the on-going program. Significant results have been obtained in defining the structure of the three-dimensional shock wave turbulent boundary layer interaction by combining detailed experiments with coordinated major computational programs. Keywords: Shock wave, Boundary layer, Supersonic.

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Document Details

Document Type
Technical Report
Publication Date
Nov 24, 1987
Accession Number
ADA187642

Entities

People

  • Seymour M. Bogdonoff

Organizations

  • Princeton University

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Boundary Layer
  • Classification
  • Contracts
  • Dynamics
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Heat Transfer
  • Pressure Distribution
  • Pressure Measurement
  • Shock Waves
  • Static Pressure
  • Three Dimensional
  • Turbulent Boundary Layer
  • Two Dimensional
  • Universities

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Joint Military Operations and Doctrine.

Technology Areas

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