A Flat Plate Study of the Binary Scaling of Viscous Hypersonic Flow.

Abstract

The interaction between the inviscid field and the large viscous boundary layer characteristic of hypersonic flow is analyzed from the continuum viewpoint. A variety of similarity parameters are derived to represent the viscous flow over slender bodies. The similitude is described by a binary collision scaling parameter, so that it is possible to apply a binary scaling that transforms density and length in inverse proportion at a fixed velocity and temperature. Experiments at a Mach number near 13 on a thermally controlled copper sharp plate were conducted to examine the wall temperature effects. Because of the wide range of test conditions covered in the experiments, the results provide some insight into viscous similarity when molecular effects begin to appear at the leading edge.

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1971
Accession Number
AD0736050

Entities

People

  • D. J. Harney
  • S. L. Petrie

Organizations

  • Ohio State University

Tags

DTIC Thesaurus Topics

  • Bodies
  • Boundaries
  • Boundary Layer
  • Collisions
  • Flow
  • Fluid Flow
  • Hypersonic Flow
  • Layers
  • Leading Edges
  • Mach Number
  • Motion
  • Physical Properties
  • Slender Bodies
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

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