Hypersonic Crossing Shock-Waves/Turbulent Boundary Layer Interaction

Abstract

This report results from a contract tasking Institute of Theoretical and Applied Mechanics as follows: The contractor will help the CFD group at AFRL to better understand shock-wave/turbulent boundary layer phenomena by providing a comprehensive set of experimental data with emphasis on both quantitative and flow visualization aspects. He will fill-in the gaps which exist in the test matrix both at Mach 4 and 5 He will also expand the range of measurements to include shock structure and skin friction coefficient data.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1999
Accession Number
ADA363672

Entities

People

  • Alexander A. Zheltovodov
  • Alexander I. Maksimov

Organizations

  • Russian Academy of Sciences

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Layers
  • Measurement
  • Physics Laboratories
  • Pressure Distribution
  • Pressure Measurement
  • Secondary Flow
  • Shock Waves
  • Skin Friction
  • Turbulent Boundary Layer
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Fluid Mechanics and Fluid Dynamics.
  • Technical Research and Report Writing.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow