Hypersonic Heat Transfer Test Program in the VKI Longshot Facility.

Abstract

The purpose of these tests was to measure local pressure and heat transfer distributions on an ogive body configuration over a range of Mach number and Reynolds number conditions. Both smooth and rough body data were obtained at three degrees angle of attack. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Dec 21, 1977
Accession Number
ADA050295

Entities

People

  • V. Dicristina

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Gages
  • Heat Energy
  • Heat Transfer
  • High Pressure
  • High Resolution
  • Mach Number
  • Measurement
  • Pressure Gages
  • Reynolds Number
  • Roughness
  • Surface Roughness
  • Test Facilities

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow