HEAT TRANSFER FROM THE REAR OF BLUFF OBJECTS TO A LOW SPEED AIR STREAM

Abstract

The local heat transfer by forced convection from the base surface of a blunt obstacle in a variety of configurations has been measured. The data are satisfactorily correlated by an equation, where the properties are evaluated at the mean film temperature. The coefficient C depends upon the configuration and the location on the rear surface. Devices that close the dead-air space, or reduce its size, reduce the value of C. Thus, C has practically the uniform value 0.20 for a flat-plate strip at 90-degree angle of attack; but at 25-degree angle of attack it changes from 0.09 sub 3, where the apparent free streamline changes direction through an obtuse angle, to 0.18 where the apparent free streamline changes direction through an acute angle.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1962
Accession Number
AD0282336

Entities

People

  • H. H. Sogin

Organizations

  • Tulane University of Louisiana

Tags

Communities of Interest

  • Air Platforms
  • Autonomy
  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Angle Of Incidence
  • Boundary Layer
  • Coefficients
  • Convection
  • Flow
  • Heat Flux
  • Heat Transfer
  • Heat Transmission
  • Mechanics
  • Reynolds Number
  • Stagnation Pressure
  • Stagnation Temperature
  • Thermal Conductivity
  • Two Dimensional
  • United States
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster