JET ENGINE NOZZLE Russian patent published in 2001 - IPC

Abstract RU 2165538 C2

FIELD: aircraft industry. SUBSTANCE: invention relates to rocket engines with outlet part curvilinear in axial section. It is advised to make above-indicated outlet part with variable- length radius in axial direction. EFFECT: provision of control of separation of flow at nozzle outlet. 3 dwg

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RU 2 165 538 C2

Authors

Jan Kheggander

Lars-Olof Pekkari

Dates

2001-04-20—Published

1996-02-12—Filed