Turbulent-Heat-Transfer Measurements at a Mach Number of 3.03

Abstract

Turbulent-heat-transfer measurements were obtained through use of a three-dimensional axially symmetric nozzle which consists of an inner shaped plug and an outer cylindrical sleeve. Measurements were taken along the outer sleeve and gave flat-plate results that are free from wall interference and corner effects for a Mach number of 3.03 and for a Reynolds number range of 5.6 x 10(exp 6) to 6.5 x 10(exp 7). The heat-transfer-coefficient results are in good agreement with theoretical analyses and the recovery-factor results are in good agreement with extrapolations of lower Reynolds number data.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1954
Accession Number
ADA377249

Entities

People

  • Bernard Rashis
  • Maurice J. Brevoort

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Boundary Layer
  • Coefficients
  • Equations
  • Free Stream
  • Heat Transfer
  • Heat Transfer Coefficients
  • Mach Number
  • Materials
  • Measurement
  • Prandtl Number
  • Reynolds Number
  • Specific Heat
  • Stagnation Temperature
  • Surface Temperature
  • Thermal Conductivity
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Electrical Engineering
  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.