EXPERIMENTAL STUDIES OF LOW-DENSITY EFFECTS IN HYPERSONIC WEDGE FLOWS

Abstract

Experimental heat transfer and pressure data are presented which extend from the classical thin boundary layer regime to near-free-molecule flow (Knudsen numbers based on ambient stream conditions as large as 5). These data are compared with viscous shock layer theory for heat transfer and with theory for the combined effects of wedge angle and boundary layer displacement to define the theoretical range of validity and to identify the low density departures from boundary layer theory. It is noted that low density effects are first evident in the pressure data. It is concluded that the cause of these departures cannot be identified within existing solutions based on the Navier- Stokes relations. It is hypothesized that the departures might stem from second- order (Burnett) molecular effects.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1964
Accession Number
AD0616898

Entities

People

  • J. A. Bartz
  • R. J. Vidal

Organizations

  • Calspan

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Boundaries
  • Boundary Layer
  • Displacement
  • Equations
  • Flow
  • Gas Flow
  • Heat Transfer
  • Hydrostatic Pressure
  • Knudsen Number
  • Leading Edges
  • Low Density
  • Mean Free Path
  • Measurement
  • Mechanics
  • Pressure Distribution
  • Pressure Gradients

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

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