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contributor authorJu Qiu
contributor authorQin Sun
date accessioned2017-05-08T21:34:20Z
date available2017-05-08T21:34:20Z
date copyrightNovember 2015
date issued2015
identifier other%28asce%29as%2E1943-5525%2E0000330.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56479
description abstractThe current work is a contribution to the potential effect of the aft fuselage stiffness modifications on the flutter characteristics of a T-tail. The rear fuselage is simulated by beam elements, based on a fixed T-tail structure. Their stiffness ranges from
publisherAmerican Society of Civil Engineers
titleT-Tail Flutter Analysis with Simulated Fuselage Stiffness
typeJournal Paper
journal volume28
journal issue6
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000328
treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 006
contenttypeFulltext


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