Research on Vibration Load Spectrum of Aero Engine Control System Based on Fatigue Damage Equivalence

Author:

Yu Danni,Lu Zepeng,Gao Yahui

Publisher

Springer Nature Singapore

Reference20 articles.

1. Cowles, B.A.: High cycle fatigue in aircraft gas turbines—an industry perspective. Int. J. Fract. 80(2–3), 147–163 (1996)

2. De Jong, J.B., Schütz, D., Lowak, H., et al.: A standardized load sequence for flight simulation tests on transport aircraft wing structures. NLR-TR 73029 U, LBF Bericht FB-106 (1973)

3. Yingdong, S., Deping, G.: Aeroengine composite maneuver loading spectrum derivation. J. Aerospace Power 02, 212–216 (2002). (in Chinese)

4. Yingdong, S., Zhigang, S.: Model and simulation of aeroengine load spectrum related to operation. J. Aerospace Power 06, 727–731 (2003). (in Chinese)

5. Yongming, Z., Yingdong, S.: Research on multi-axial fatigue test loading spectrum formation based on damage equivalent principle. J. Aerospace Power 24(09), 2026–2032 (2009). (in Chinese)

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