Zobrazeno 1 - 2
of 2
pro vyhledávání: '"Lin, Yongchen"'
Publikováno v:
In Aerospace Science and Technology March 2019 86:177-190
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:563-572
The dual throat nozzle achieves higher thrust vectoring efficiencies and lesser thrust loss than other fluidic thrust-vectoring nozzles. Separation always occurs at the bottom of the cavity with complex three-dimensional characteristics for the dual