THE FLOW OVER A CYLINDER WITH VARIOUS NOSE SHAPES AT ZERO ANGLE OF ATTACK AT HYPERSONIC SPEEDS

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1963
Accession Number
AD0299261

Entities

People

  • C.c. Horstman

Organizations

  • Princeton University

Tags

Technology Areas

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