Study on modal characteristics and vibration reduction of an aircraft rotor–stator brake-induced squeal system
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Computational Mechanics
Link
https://link.springer.com/content/pdf/10.1007/s10409-020-01003-9.pdf
Reference30 articles.
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3. Knowles, J.A.C., Krauskopf, B., Lowenberg, M.H., et al.: Numerical continuation analysis of a dual-sidestay main landing gear mechanism. J. Aircraft 51(1), 129–143 (2014). https://doi.org/10.2514/1.c032130
4. Shang, Y.X., Liu, X.C., Jiao, Z.X., et al.: A novel integrated self-powered brake system for more electric aircraft. Chin. J. Aeronaut. 31(5), 976–989 (2018). https://doi.org/10.1016/j.cja.2017.11.015
5. Fan, S., Zhang, L., Cheng, L., et al.: Effect of braking pressure and braking speed on the tribological properties of C/SiC aircraft brake materials. Compos. Sci. Technol. 70(6), 959–965 (2010). https://doi.org/10.1016/j.compscitech.2010.02.012
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