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TUNNEL SUPERSONIQUE ECOULEMENT INTERMITTENT [1 record]

Record 1 2008-09-30

English

Subject field(s)
  • Aerodynamics and Theory of Gases
  • Aeronautical Engineering and Maintenance
CONT

The Mach number and temperature calibration of an axisymmetric, intermittent-flow supersonic wind tunnel. ... Static pressure and temperature surveys were conducted in the 4.5-inch diameter, axisymmetric, intermittent-flow, supersonic wind tunnel to determine the flow characteristics.

Key term(s)
  • intermittent flow supersonic wind tunnel

French

Domaine(s)
  • Théorie des gaz et aérodynamique
  • Aérotechnique et maintenance
OBS

Fonctionnant dans des régimes d’écoulement subsonique, transsonique et supersonique, à des vitesses allant de Mach 0,1 à plus de Mach 4, l’installation d’écoulement intermittent pressurisée constitue un endroit idéal pour l’essai de modèles dans diverses conditions.

Spanish

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