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TsAGI Science Journal

ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.2014012229
pages 451-462

EXPERIMENTAL INVESTIGATION OF INTEGRAL PROPULSION SYSTEM PERFORMANCE FOR A BLENDED-WING-BODY CONFIGURATION

Vladimir Ivanovich Vasiliev
Central Aerohydrodynamic Institute (TsAGI), 1 Zhukovsky Str., Zhukovsky 140180, Russia
Gennadii Nikolaevich Lavrukhin
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia
Valerii Vladimirovich Lazarev
Central Aerohydrodynamic Institute (TsAGI), Zhukovsky str. 1, Zhukovsky, 140180, Russia
Gennadii Pavlovich Noskov
Central Aerohydrodynamic Institute (TsAGI), 1 Zhukovsky Str., Zhukovsky 140180, Russia
Vadim Alekseevich Talyzin
Central Aerohydrodynamic Institute (TsAGI), 1 Zhukovsky Str., Zhukovsky 140180, Russia

RÉSUMÉ

Results of experimental investigations of the performance of a propulsion system integrated into a large-scale blended-wing-body model are presented. The characteristics of the inlet and nozzle during their simultaneous operation are measured and the flow is visualized at the incoming flow velocity V = 0 − 120 m/s and different angles of attack.


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