Second-Order Theory of Optimum Two-Dimensional Wings in Supersonic Flow Including the Effects of Friction

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1963
Accession Number
AD0420810

Entities

People

  • Angelo Miele
  • Arthur H. Lusty

Organizations

  • Boeing

Tags

DTIC Thesaurus Topics

  • Flow
  • Fluid Flow
  • Friction
  • Gas Flow
  • Geometry
  • Supersonic Flow
  • Two Dimensional

Technology Areas

  • Hypersonics