A NOTE ON THE CORRECTING OF MEASURED PRESSURES FOR FREE-STREAM FLOW GRADIENTS IN HYPERSONIC FLOW,

Abstract

The effect of free-stream flow gradients upon the pressures measured along a thin body was studied. An expansion procedure using the Mach number gradient as the expansion parameter was used to determine the effect of these gradients upon the pressures measured on a wedge. These results were then used to determine the effect of the flow gradients upon other bodies, in particular, a flat plate with a blunted leading edge. A comparison with experimental and exact calculated values indicates that this method is in better agreement with the uniform flow pressure distribution than the methods presently in use. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1962
Accession Number
AD0627423

Entities

People

  • R. A. Makofski

Organizations

  • Johns Hopkins University Applied Physics Laboratory

Tags

DTIC Thesaurus Topics

  • Agreements
  • Flow
  • Fluid Flow
  • Free Stream
  • Gas Flow
  • Hypersonic Flow
  • Leading Edges
  • Mach Number
  • Physical Properties
  • Pressure Distribution

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Linear Algebra

Technology Areas

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