Second-Order Compressible Boundary-Layer Theory with Application to Blunt Bodies in Hypersonic Flow,

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1961
Accession Number
AD0267859

Entities

People

  • Milton Van Dyke

Organizations

  • Stanford University

Tags

DTIC Thesaurus Topics

  • Blunt Bodies
  • Bodies
  • Boundaries
  • Boundary Layer
  • Flow
  • Hypersonic Flow
  • Layers

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers