A structural and thermal study of an oscillating vibration damper Online publication date: Mon, 09-Jun-2014
by Thomas S. Miller, John C. Tunney, David E. Roth
International Journal of Computer Applications in Technology (IJCAT), Vol. 7, No. 3/4/5/6, 1994
Abstract: An elastomeric vibration damper experiencing cyclic loading within a helicopter rotor blade assembly is analysed to better understand its thermal characteristics. Experimental testing shows that elevated temperatures contribute to the degradation of the elastomer and adhesive system, shortening service life. The statistical approach of 'Designed Experimentation' is used to combine numerous design and environmental variables to find maximum temperatures within the damper. Both structural and thermal finite element analyses are used within the designed experiment to determine high temperatures of the damper for each of several trials. The designed experiment then ranks each variable in order of importance in creating high temperatures within the damper.
Existing subscribers:
Go to Inderscience Online Journals to access the Full Text of this article.
If you are not a subscriber and you just want to read the full contents of this article, buy online access here.Complimentary Subscribers, Editors or Members of the Editorial Board of the International Journal of Computer Applications in Technology (IJCAT):
Login with your Inderscience username and password:
Want to subscribe?
A subscription gives you complete access to all articles in the current issue, as well as to all articles in the previous three years (where applicable). See our Orders page to subscribe.
If you still need assistance, please email subs@inderscience.com