NOL HYPERSONIC TUNNEL NO. 4 - RESULTS VI: - EXPERIMENTAL AND THEORETICAL INVESTIGATION OF THE BOUNDARY LAYER AND HEAT TRANSFER CHARACTERISTICS OF A COOLED HYPERSONIC WEDGE NOZZLE AT A MACH NUMBER OF 5.5

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Document Details

Document Type
Technical Report
Publication Date
Jul 08, 1954
Accession Number
AD0045969

Entities

People

  • E. M. Winkler
  • Jerome Persh

Organizations

  • Naval Ordnance Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Equations
  • Experimental Data
  • Flow
  • Fluid Dynamics
  • Fluid Mechanics
  • Free Stream
  • Heat Transfer
  • Jet Propulsion
  • Mach Number
  • Munitions
  • Physics Laboratories
  • Pressure Gradients
  • Reynolds Number
  • Temperature Gradients
  • Turbulent Flow

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow