A METHOD FOR CALCULATING TURBULENT BOUNDARY LAYER DEVELOPMENT IN SUPERSONIC AND HYPERSONIC NOZZLES INCLUDING THE EFFECTS OF HEAT TRANSFER

Document Details

Document Type
Technical Report
Publication Date
Jun 07, 1956
Accession Number
AD0101927

Entities

People

  • Jerome Persh
  • Roland Lee

Organizations

  • Naval Ordnance Laboratory

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Heat Transfer
  • Hypersonic Nozzles
  • Layers
  • Nozzles
  • Turbulent Boundary Layer

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow