Experimental Investigation of The Hemisphere-Cylinder At Hypervelocities In Air

Abstract

Pressure, heat transfer, drag, and shock detachment data were obtained for a hemisphere-cylinder model in the GDF Hotshot I hypervelocity wind tunnel.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1958
Accession Number
AD0204392

Entities

People

  • J. C. Boison

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Boundary Layer
  • Bow Shock
  • Dynamic Pressure
  • Free Stream
  • Heat Transfer
  • Instrumentation
  • Mach Number
  • Measurement
  • Photographs
  • Pressure Distribution
  • Pressure Measurement
  • Pressure Transducers
  • Skin Friction
  • Static Pressure
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow