Problem of Supersonic Flow Declaration by Magnetic Field

Abstract

This report results from a contract tasking Central Institute of Aviation Motors as follows: The contractor will investigate the problem of hypersonic flow control by magnetic field in channels with minimal losses.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1997
Accession Number
ADA336189

Entities

People

  • Alexander B. Vatazhin
  • E. K. Kholshchevikova
  • O. V. Gouskov
  • V. A. Likhter
  • V. I. Kopchenov

Organizations

  • Baranov Central Institute of Aviation Motor Development

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Contracts
  • Electric Current
  • Electric Fields
  • Electromagnetic Fields
  • Energy Production
  • Euler Equations
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Hypersonic Flow
  • Hypervelocity Flow
  • Magnetic Fields
  • Propulsion Systems
  • Steady State
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Plasma Physics / Magnetohydrodynamics
  • Technical Research and Report Writing.

Technology Areas

  • Hypersonics