SURVEY OF FRICTION COEFFICIENTS, RECOVERY FACTORS, AND HEAT-TRANSFER COEFFICIENTS FOR SUPERSONIC FLOW

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1953
Accession Number
AD0020190

Entities

People

  • Joseph Kaye

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms

DTIC Thesaurus Topics

  • Boundary Layer
  • Compressible Flow
  • Computational Fluid Dynamics
  • Fluid Dynamics
  • Fluid Mechanics
  • Heat Transfer
  • Heat Transfer Coefficients
  • Laminar Boundary Layer
  • Mach Number
  • Measurement
  • Mechanical Engineering
  • Prandtl Number
  • Pressure Gradients
  • Reynolds Number
  • Skin Friction
  • Turbulent Boundary Layer
  • Two Dimensional

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight