AN INEXPENSIVE SUPERSONIC WIND TUNNEL FOR HEAT-TRANSFER MEASUREMENTS. PART 1. APPARATUS, DATA, AND RESULTS FOR A LAMINAR BOUNDARY LAYER BASED ON A SIMPLE ONE-DIMENSIONAL FLOW MODEL

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1954
Accession Number
AD0045686

Entities

People

  • George A. Brown
  • Joseph Kaye
  • Joseph. H. Keenan
  • Robert H. Shoulberg

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundary Layer
  • Fluid Mechanics
  • Heat Transfer
  • Heat Transfer Coefficients
  • Laminar Boundary Layer
  • Mechanical Engineering
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Stagnation Temperature
  • Static Pressure
  • Steady State
  • Supersonic Wind Tunnels
  • Temperature Gradients
  • Thermal Conductivity
  • Turbulent Boundary Layer
  • Wind Tunnels

Technology Areas

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