A SIMPLIFIED ANALYSIS OF VECTORIAL INJECTION IN HYPERSONIC FLOW.

Abstract

The equations relating to laminar binary boundary layer flow are solved approximately, in accordance with the boundary conditions for vectorial injection. Expressions for the skin friction and heat transfer coefficients are derived, together with their normalized representations. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1965
Accession Number
AD0615326

Entities

People

  • Philip S. Kirk

Organizations

  • University of Cincinnati

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Boundary Layer Flow
  • Coefficients
  • Equations
  • Flow
  • Friction
  • Heat Transfer
  • Heat Transfer Coefficients
  • Hypersonic Flow
  • Layers
  • Skin Friction

Readers

  • Calculus or Mathematical Analysis
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers