A THEORETICAL INVESTIGATION OF THE EFFECT ON INJECTION OF AIR ON TURBULENT BOUNDARY LAYER SKIN-FRICTION AND HEAT-TRANSFER COEFFICIENTS AT SUPERSONIC AND HYPERSONIC SPEEDS

Document Details

Document Type
Technical Report
Publication Date
Jan 04, 1957
Accession Number
AD0125709

Entities

People

  • Jerome Persh

Organizations

  • Naval Ordnance Laboratory

Tags

DTIC Thesaurus Topics

  • Boundary Layer
  • Coefficients
  • Friction
  • Heat Transfer
  • Heat Transfer Coefficients
  • Skin Friction
  • Turbulent Boundary Layer

Technology Areas

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