Symmetric and Asymmetric Crossing-Shock-Waves/Turbulent Boundary Layer Interactions

Abstract

This report results from a contract tasking Institute of Theoretical and Applied Mechanics as follows: The contractor will analyze experimental data (obtained at ITAM) such as surface flow visualization, surface pressure, adiabatic wall temperature and surface heat transfer for symmetric and asymmetric crossing shock waves/turbulent boundary layer interactions as detailed in his proposal submitted in April 97.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1998
Accession Number
ADA353759

Entities

People

  • Alexander A. Zheltovodov
  • Alexander I. Maksimov

Organizations

  • Russian Academy of Sciences

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Geometry
  • Heat Transfer
  • Hydrodynamics
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Secondary Flow
  • Shock Waves
  • Three Dimensional
  • Turbulent Boundary Layer
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Technical Research and Report Writing.