Hypersonic Wake Semiannual Report

Abstract

Primary emphasis is placed on the solution to the near wake viscous interaction problem by both the integral and finite difference methods. Results of the rotational characteristics program with the inclusion of shock waves are also presented.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1966
Accession Number
AD0484690

Entities

People

  • Leslie A. Hromas

Organizations

  • TRW Inc.

Tags

Communities of Interest

  • Air Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Boundary Layer
  • California
  • Compression Waves
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Governments
  • Inviscid Flow
  • Mach Number
  • Pressure Gradients
  • Reynolds Number
  • Shock Waves
  • Stagnation Point
  • Turbulent Mixing
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Fluid Dynamics.
  • Technical Research and Report Writing.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight