High-Fidelity Simulation and Performance Analysis of Twin-Spool Turbofan Engine Based on Multi-dynamics Approach-Reference-Cited by-同舟云学术

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High-Fidelity Simulation and Performance Analysis of Twin-Spool Turbofan Engine Based on Multi-dynamics Approach

Published:2024-05-18 Issue: Volume: Page:
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Guo Chaochao,Sun Youchao,Li Longbiao,Zhu Xiaodong

Funder

Innovative Research Group Project of the National Natural Science Foundation of China

the Joint Fund of National Natural Science Foundation of China and Civil Aviation Administration of China

Fundamental Research Funds for the Central Universities

Publisher

Springer Science and Business Media LLC

Link

https://link.springer.com/content/pdf/10.1007/s42405-024-00748-y.pdf

Reference29 articles.

1. Dou J, Huang J, Zhou W (2005) Research of aeroengine modeling based on UML. J Aerosp Power 20:684–688

2. Sun L, Sun J, Zhang H (2009) Software componentization modeling for aero-engines. J Aerosp Power 24:2368–2371

3. Lytle JK (2000) The numerical propulsion system simulation: an overview. Comput Aerosci 2000:1

4. Naiman CG (2004) Numerical propulsion system simulation architecture. In: 40th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, NASA, Cleveland

5. Jones SM (2007) An introduction to thermodynamic performance analysis of aircraft gas turbine engine cycles using the numerical propulsion system simulation code

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