PITOT-PRESSURE MEASUREMENTS WITH RAPIDLY TRAVERSING PROBES IN THE WAKE OF A SPHERE IN A DIVERGING HYPERVELOCITY STREAM

Abstract

Contents: Apparatus and test conditions; Transducer-galvanometer response and correction; Source-flow effects and correction; Data reduction and results.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1968
Accession Number
AD0672589

Entities

People

  • Denis W. Tsao

Organizations

  • Stanford University

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Flow Fields
  • Fluid Dynamics
  • Fluid Mechanics
  • Geometry
  • Hydrodynamics
  • Inviscid Flow
  • Mach Number
  • Measurement
  • Pitot Tubes
  • Pressure Distribution
  • Pressure Measurement
  • Pressure Transducers
  • Shock Tubes
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

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