TsAGI Science Journal
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ISSN Печать: 1948-2590
ISSN Онлайн: 1948-2604
EXPERIMENTAL INVESTIGATION OF THE AEROGASDYNAMICS OF A VECTORED-THRUST NOZZLE
Том 45,
Выпуск 7, 2014,
pp. 659-667
DOI: 10.1615/TsAGISciJ.2014012972
Краткое описание
The results of the flow visualization and investigation of the aerogasdynamics characteristics of a turbofan engine nozzle with a thrust-vector control are presented. Some peculiarities of the flow and alteration of the nozzle characteristics with jet deflection are founded.
Ключевые слова: turbofan, nozzle, thrust vectoring, subsonic flow, thrust losses, thrust vector angle
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