Design and Investigation of a Three-Dimensional TBCC Exhaust System Operating at Mach 0–6

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Date
2026
Author
Lv, Zheng
Ye, Tao
Ding, Haipeng
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Abstract
AbstractThis study presents the design and investigation of a three-dimensional (3D) turbine-based combined cycle (TBCC) exhaust system operating across Mach 0 to 6. The streamline tracing technique is utilized to design the 3D asymmetric nozzle for the ...
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http://yetl.yabesh.ir/yetl1/handle/yetl/4314117
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