General Design Method of Control Law for Adaptive Cycle Engine Mode Transition-Reference-Cited by-同舟云学术

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General Design Method of Control Law for Adaptive Cycle Engine Mode Transition

Published:2021-08-23 Issue: Volume: Page:1-15
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zhang Jiyuan¹^ORCID,Dong Pengcheng²,Tang Hailong³,Zheng Junchao⁴,Wang Jingkai⁵,Chen Min¹

Affiliation:

1. Beihang University, 100191 Beijing, People’s Republic of China

2. Aero Engine Academy of China, 101304 Beijing, People’s Republic of China

3. Beihang University, 102206 Beijing, People’s Republic of China

4. Tsinghua University, 100084 Beijing, People’s Republic of China

5. AVIC Shenyang Engine Research Institute, 110015 Shenyang, Liaoning, People’s Republic of China

Funder

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060674

Reference34 articles.

1. Progress in Aeroengine Technology (1939--2003)

2. Progress in Astronautics and Aeronautics;Johnson J. E.,1996

3. Exergetic sustainability off-design analysis of variable-cycle aero-engine in various bypass modes

4. BuettnerR. W.RobertsR.WolffM. “Design of a Transient Variable Cycle Turbine Engine Model for System Integration with Controls,” AIAA Paper 2017-1940, Jan. 2017. 10.2514/6.2017-1940

5. Analysis of aerodynamic/propulsive couplings during mode transition of over-under turbine-based-combined-cycle engines

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