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TsAGI Science Journal

ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.2017019841
pages 747-758

DEVELOPMENT OF THE CONCEPT OF CURVILINEAR CHANNELS FOR PROPULSION SYSTEM INLETS AND NOZZLES EMBEDDED IN THE AIRFRAME

Oleg Petrovich Minin
Tupolev Design Bureau, 17 Academician Tupolev Embankment, Moscow, 105005, Russian Federation
Sergei Grigorievich Shevel'kov
Tupolev Design Bureau, 17 Academician Tupolev Embankment, Moscow, 105005, Russian Federation
Vasilii Pavlovich Shpagin
Tupolev Design Bureau, 17, Academician Tupolev Embankment, Moscow, 105005, Russia
Nadezhda Yurievna Yurlova
Tupolev Design Bureau, 17, Academician Tupolev Embankment, Moscow, 105005, Russia

ABSTRAKT

The propulsion airframe integrated configuration of a tailless aircraft is considered in this study. Several concepts of embedded inlets and nozzles are presented. The results of the numerical flow simulation in the presented inlets and nozzles are obtained.


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