Hypersonic Shock Tunnel Performance Characteristics.

Abstract

The desired goal was to state the initial conditions and throat diameters which are suitable for testing re-entry shape models or hypersonic glide shapes in the shock tunnel.

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1974
Accession Number
ADA023542

Entities

People

  • Douglas H. May

Organizations

  • Air Force Institute of Technology

Tags

DTIC Thesaurus Topics

  • Blast Tubes
  • Buildings And Structures
  • Diameters
  • Geometry
  • Mathematics
  • Physical Properties
  • Shock Tubes
  • Shock Tunnels
  • Sizes (Dimensions)

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow