RESULTS OF INDEPENDENT RESEARCH AND DEVELOPMENT STUDIES BY THE DOUGLAS AEROPHYSICS LABORATORY STAFF IN FLUID MECHANICS AND SIMULATION TECHNIQUES FISCAL YEAR 1962

Abstract

Contents: Experimental work on transition at hypersonic speeds Hypersonic turbulent heat transfer Hypervelocity studies using hypervelocity impulse tunnel Hypervelocity studies using light gas gun and ballistic range Transonic test section studies Wind tunnel investigations of a 1/16 scale model of the proposed annular steam ejector for the trisonic four/foot wind tunnel Hypersonic wind tunnel instrumentation studies Flow investigations in the hypersonic wind tunnel Optical flow visualization instrumentation

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1963
Accession Number
AD0403107

Entities

People

  • W. E. Smith

Organizations

  • Douglas

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Closed Bomb Tests
  • Flow Visualization
  • Fluid Mechanics
  • Geometry
  • Heat Transfer
  • Jet Propulsion
  • Measurement
  • Mechanics
  • Optics
  • Pressure Distribution
  • Pressure Measurement
  • Shock Tunnels
  • Strain Gages
  • Telemetry Equipment
  • Test And Evaluation
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow