Low-emission optimization control method for coaxial compound helicopter/engine based on variable geometry adjustment-Reference-Cited by-同舟云学术

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Low-emission optimization control method for coaxial compound helicopter/engine based on variable geometry adjustment

Published:2024-08 Issue: Volume:151 Page:109263
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Song Jie^ORCID,Li Shancheng,Zhu Shicheng,Wang Yong,Zhang Haibo

Publisher

Elsevier BV

Reference41 articles.

1. Pollutant emissions from gas fired turbine engines in offshore practice: measurements and scaling;Røkke,1993

2. Air Transport and the Environment;Daley,2016

3. Optimum problems in environmental emissions of aircraft arrivals;Zhang;Aerosp. Sci. Technol.,2022

4. Nitrogen dioxide formation in gas turbine engines: measurements and measurement methods;Tuttle;Combust. Sci. Technol.,1974

5. A minimum objective function trim procedure for VTOLs noise reduction;Poggi;Aerosp. Sci. Technol.,2024

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Neural Network Signal Integration from Thermogas-Dynamic Parameter Sensors for Helicopters Turboshaft Engines at Flight Operation Conditions;Sensors;2024-06-29

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