Receptivity of Hypersonic Boundary Layer to Acoustic Disturbances Scattered by Surface Roughness

Abstract

This report results from a contract tasking Moscow Institute of Physics and Technology as follows: The contractor will perform theoretical analysis on the receptivity of hypersonic boundary layer to acoustic disturbances as outlined in his proposal submitted in May 98.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1999
Accession Number
ADA367489

Entities

People

  • Alexander V. Fedorov

Organizations

  • Moscow Institute of Physics and Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Acoustic Waves
  • Boundaries
  • Boundary Layer
  • Boundary Layer Flow
  • Dispersion Relations
  • Flow Fields
  • Fluid Dynamics
  • Frequency
  • Layers
  • Leading Edges
  • Mach Number
  • Reynolds Number
  • Roughness
  • Surface Roughness
  • Three Dimensional
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

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

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers