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Study on integrated control for supersonic inlet and turbofan engine model
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.1 ) Pub Date : 2020-07-27 , DOI: 10.1177/0954410020944068 Haoying Chen 1 , Haibo Zhang 1 , Yao Du 1 , Qiangang Zheng 1
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.1 ) Pub Date : 2020-07-27 , DOI: 10.1177/0954410020944068 Haoying Chen 1 , Haibo Zhang 1 , Yao Du 1 , Qiangang Zheng 1
Affiliation
Considering the supersonic inlet model with normal shock position feedback, the integrated control method of inlet and turbofan engine is studied. The integrated model includes the supersonic inlet...
中文翻译：
超音速进气涡扇发动机模型集成控制研究
考虑具有正常冲击位置反馈的超音速进气模型，研究了进气涡扇发动机的集成控制方法。集成模型包括超音速进气...
更新日期：2020-07-27
中文翻译：
超音速进气涡扇发动机模型集成控制研究
考虑具有正常冲击位置反馈的超音速进气模型，研究了进气涡扇发动机的集成控制方法。集成模型包括超音速进气...
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