Test Research and Finite Element Analysis on Extension Performance of Civil Aircraft Flaps Subjected to Extreme Temperature
Author:
Publisher
Springer Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-33-6060-0_1
Reference17 articles.
1. Heyden T Elastic multibody models of transport aircraft high-lift mechanisms. J Aircraft 46(5):1513–1524
2. Chunlin G et al (2018) Numerical investigation of the effects of different parameters on the thrust performance of three dimensional flapping wings. Aerospace Sci Technol
3. Song Q (2017) Analysis of flap mechanism reliability. In: International conference on mechatronics engineering & information technology
4. Renukumar B et al Effect of flap and slat riggings on 2-D high-lift aerodynamics. J Aircraft. 43(5):1259–1271
5. Cui L, Lu Z, Hao W Importance analysis of the aircraft flap mechanism movement failure. J Aircraft 48(2):606–611
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