Predictive control method for mode transition process of multi-mode turbine engine based on onboard adaptive composite model-Reference-Cited by-同舟云学术

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Predictive control method for mode transition process of multi-mode turbine engine based on onboard adaptive composite model

Published:2024-09 Issue: Volume:302 Page:131748
ISSN:0360-5442
Container-title:Energy
language:en
Short-container-title:Energy

Author:

Cai Changpeng^ORCID,Zheng Qiangang^ORCID,Wang Yong,Chen Haoying,Zhang Haibo

Publisher

Elsevier BV

Reference39 articles.

1. A review of design issues specific to hypersonic flight vehicles;Sziroczak;Prog Aero Sci,2016

2. Exergetic sustainability off-design analysis of variable-cycle aero-engine in various bypass modes;Aygun;Energy,2020

3. Energy and performance optimization of an adaptive cycle engine for next generation combat aircraft;Aygun;Energy,2020

4. Technical approach to turbine-based combined cycle: FaCET[C];Mamplata,2009

5. Hypersonic wavecatcher intakes and variable-geometry turbine based combined cycle engines;Zuo;Prog Aero Sci,2019

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1. Prediction of engine combustion chamber outlet temperature field based on deep Learning: Application in aero-engine life extension control;Applied Thermal Engineering;2024-10

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