HEAT TRANSFER MEASUREMENTS ON A CONE-CYLINDER-FLARE AT A MACH NUMBER OF 6.8

Abstract

Heat transfer measurements have been made in the hypersonic wind tunnel on a cone-cylinder-flare and high values of the heat transfer factor found where the flow reattached on the flare.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1962
Accession Number
AD0331849

Entities

People

  • A. Naysmith

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Equations
  • Errors
  • Flow
  • Heat Transfer
  • Heat Transmission
  • Hypersonic Wind Tunnels
  • Instrumentation
  • Low Drag
  • Mach Number
  • Measurement
  • Measuring Instruments
  • Photographs
  • Pressure Measurement
  • Stagnation Temperature
  • Thermal Conductivity
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

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