Journal of Engineering and Applied Sciences

Year: 2019
Volume: 14
Issue: 11
Page No. 3571 - 3574

Vibration Analysis of Aircraft Wing under Gust Load

Authors : Majid Habeeb Faidh-Allah and Adawiya Ali Hamzah

References

Anonymous, 2014. ANSYS user manual (version 15.0). Ansys, Canonsburg, Pennsylvania, USA.

Chudy, P., 2004. Response of a light aircraft under gust loads. Acta Polytech., 44: 97-102.
Direct Link  |  

Das, S., J. Baral and P. Chatterjee, 2011. Active vibration control of piezo-laminated cantilever beam. Ph.D Thesis, National Institute of Technology, Rourkela, Rourkela, India.

Hamzah, A.A., 2017. Vibrational behavior of three floors structure equipped with dampers. Intl. J. Mech. Mechatron. Eng., 17: 76-85.
Direct Link  |  

Parameswaran, A.P., A.B. Pai, P.K. Tripathi and K.V. Gangadharan, 2013. Active vibration control of a smart cantilever beam on general purpose operating system. Defence Sci. J., 63: 413-417.
Direct Link  |  

Rahman, N.U. and M.N. Alam, 2012. Active vibration control of a piezoelectric beam using PID controller. Latin Am. J. Solids Struct., 9: 657-673.
CrossRef  |  Direct Link  |  

Waghulde, K.B., B. Sinha, M.M. Patil and S. Mishra, 2010. Vibration control of cantilever smart beam by using piezoelectric actuators and sensors. Intl. J. Eng. Technol., 2: 259-262.
Direct Link  |  

Design and power by Medwell Web Development Team. © Medwell Publishing 2024 All Rights Reserved