Thrust control strategy based on the minimum combustor...

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Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering 2019 / 02

Thrust control strategy based on the minimum combustor inlet Mach number to enhance the overall performance of a scramjet engine

Ji, Zifei, Zhang, Huiqiang, Wang, Bing
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Journal:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
DOI:
10.1177/0954410019830816
Date:
February, 2019
File:
PDF, 1.12 MB
2019
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