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AERODYNAMIC CHOKE [1 record]

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Record 1 2002-12-23

English

Subject field(s)
  • Launchers (Astronautics)
CONT

In this study, a hydraulic analog/gas flow model of a 2-d ejector has been used mainly to locate and understand the structure of the inviscid multiple stream flow (principally the location of the aerodynamic choke).

French

Domaine(s)
  • Lanceurs (Astronautique)
DEF

Phénomène causé par un flux radial de gaz dans le centre d'un propulseur.

Spanish

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