Design and performance analysis of an exhaust system for an...

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Aerospace Science and Technology 2019 / 9

Design and performance analysis of an exhaust system for an over-under turbine based combined cycle operating at Mach 0–6

Lv, Zheng, Xu, Jinglei, Song, Guangtao
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Language:
english
Journal:
Aerospace Science and Technology
DOI:
10.1016/j.ast.2019.105386
Date:
September, 2019
File:
PDF, 8.47 MB
english, 2019
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