Two-Dimensional Supersonic Wind Tunnel Investigations of Flow in a Duct with Flutuating Exit Pressure. Part 1. Experimental Technique.

Document Details

Document Type
Technical Report
Publication Date
Jun 30, 1947
Accession Number
ADA952969

Entities

People

  • M. Kamrass

Organizations

  • Calspan

Tags

DTIC Thesaurus Topics

  • Buildings And Structures
  • Geometry
  • Supersonic Wind Tunnels
  • Test Facilities
  • Two Dimensional
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow