SEPARATED FLOW STUDIES AT HYPERSONIC SPEEDS. PART II. TWO-DIMENSIONAL WEDGE SEPARATED FLOW STUDIES,

Abstract

The paper describes an experimental study of the flow patterns and distribution of heat transfer developed in regions of adverse pressure gradient and separated flow over two-dimensional models. The investigation was directed towards obtaining information on two basic problems, the separation and the reattachment of a laminar boundary layer.

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1964
Accession Number
AD0613463

Entities

People

  • Michael Holden

Organizations

  • Calspan

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Heat Transfer
  • Laminar Boundary Layer
  • Layers
  • Pressure Distribution
  • Pressure Gradients
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Business Analytics
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

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