FORCED CONVECTIVE HEAT TRANSFER TO COOLED CYLINDERS AT LOW REYNOLDS NUMBERS AND WITH LARGE TEMPERATURE DIFFERENCES

Abstract

For the purpose of determining a general correlation for forced convective heat transfer coefficients for circular cylinders in cross-flow under conditions pertaining to cooled-film application for measurements in flames and hypersonic wakes, heat transfer measurements were obtained under simulated conditions created in a plasma-jet. Measurements were made by means of constant temperature, internally cooled, cylindrical film sensors in the Reynolds number range 5-75 for various temperature loadings, the maximum being T sub infinity/T sub s = 4, and for flows composed of He, N2 and CO2. The plasma-jet conditions were maintained such that at the points of measurements, i.e. at the potential core of the jet, ionization was negligible, recombination was complete and the turbulence intensity was low. All the fluid property values in the dimensionless parameters were evaluated at the arithmetic mean temperature. A kinematic viscosity ratio instead of the more usual temperature ratio was considered in the temperature loading factor to account for the different dependency of the transport properties on temperature for different gas species. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1968
Accession Number
AD0690330

Entities

People

  • A. M. Ahmed

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Control Panels
  • Energy
  • Flow Rate
  • Fluid Mechanics
  • Gas Flow
  • Heat Transfer
  • Heat Transfer Coefficients
  • Heat Transmission
  • High Temperature
  • Measurement
  • Plasma Jets
  • Prandtl Number
  • Reynolds Number
  • Statistical Analysis
  • Thermal Conductivity
  • Transport Properties

Readers

  • Combustion science or combustion engineering.
  • Fluid Mechanics and Fluid Dynamics.
  • Plasma Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight