Mission segment division of the whole aeroengine loading spectrum based on flight actions-Reference-Cited by-同舟云学术

Mission segment division of the whole aeroengine loading spectrum based on flight actions

Published:2022-02 Issue:2 Volume:35 Page:164-174
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

JIN Yu,SUN Zhigang,SONG Yingdong,LIN Xin,NIU Xuming,DING Junjie

Funder

Nanjing University of Aeronautics and Astronautics

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference26 articles.

1. Gong J. Research on the influence of service load on the life and reliability of an aeroengine[dissertation]. Chengdu: University of Electronic Science and Technology; 2012 [Chinese].

2. General Armament Department of the Chinese People's Liberation Army.General specification for engine, aircraft, turbojet and turbofan: GJB241-2010; 2010 [Chinese].

3. US-NAVY .General specification for engine, aircraft, turbojet and turbofan: MIL-E-5007D; 1973.

4. Engine Structural Integrity Program (ENSIP) :MIL-STD-1783; 1984.

5. Ma SY, Zhang YF. Overview of aeroengine loading spectrum. Mod Mach 2011(5):15–7 [Chinese].

Cited by 4 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. Compilation Method of Flight Service Environment Spectrum Based on Altitude Features and Fuzzy Clustering;Applied Sciences;2024-06-21

2. The whirl direction and characteristics of rotor system under maneuvering flight;Vibroengineering Procedia;2023-09-21

3. Statistical Algorithms with Phase-Sensitive Detection for the Number of Hovers and S Turns in Aircraft Flights;Applied Sciences;2023-08-20

4. Counting algorithms with phase sensitive detection for hover and S turn of aircraft flight;2023-06-26