%0 Journal Article %A Vasiliev, Vladimir Ivanovich %A Lavrukhin, Gennadii Nikolaevich %A Lazarev, Valerii Vladimirovich %A Noskov, Gennadii Pavlovich %A Talyzin, Vadim Alekseevich %D 2014 %I Begell House %K blended-wing-body, propulsion system, model, inlet, nozzle, thrust loss, total pressure recovery coefficient, pressure distribution, wind tunnel, supercirculation %N 5 %P 451-462 %R 10.1615/TsAGISciJ.2014012229 %T EXPERIMENTAL INVESTIGATION OF INTEGRAL PROPULSION SYSTEM PERFORMANCE FOR A BLENDED-WING-BODY CONFIGURATION %U https://www.dl.begellhouse.com/journals/58618e1439159b1f,3c4473d2455bcb57,1c215bff3743902c.html %V 45 %X 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. %8 2014-12-29