Problems of Wind Tunnel Design and Testing.

Abstract

;Contents: Some considerations of future low-speed tunnels for Europe; Project study of a large European transonic Ludwieg tube windtunnel; The development of an efficient and economical system for the generation of quiet transonic flows suitable for model testing at high Reynolds number; The injector driven tunnel; Soufflerie a compresseur hydraulique; Facilities for aerodynamic testing at hypersonic speeds.

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1973
Accession Number
AD0774350

Entities

Organizations

  • AGARD

Tags

DTIC Thesaurus Topics

  • Blast Tubes
  • Buildings And Structures
  • Demographic Cohorts
  • Flow
  • Fluid Dynamics
  • Fluid Flow
  • Injectors
  • Research Facilities
  • Reynolds Number
  • Shock Tubes
  • Shock Tunnels
  • Test Facilities
  • Transonic Flow
  • Tubes
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Small Business Innovation Research Program (SBIR) EDI Research and Innovation.
  • Systems Analysis and Design

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow