MEASUREMENTS OF FRICTION COEFFICIENTS FOR SUPERSONIC FLOW OF AIR IN THE ENTRANCE REGION OF A TUBE WITH AND WITHOUT HEAT TRANSFER

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1953
Accession Number
AD0020189

Entities

People

  • Joseph Kaye
  • Tau-yi Toong

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Fluid Flow
  • Fluid Mechanics
  • Free Stream
  • Heat Transfer
  • Hydrodynamics
  • Laminar Boundary Layer
  • Laminar Flow
  • Mach Number
  • Mechanical Engineering
  • Mechanics
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Supersonic Flow

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow