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contributor authorTing Nung Shiau
contributor authorS. J. Chang
date accessioned2017-05-08T21:15:38Z
date available2017-05-08T21:15:38Z
date copyrightApril 1991
date issued1991
identifier other%28asce%290893-1321%281991%294%3A2%28127%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44701
description abstractThe optimal design of rotating pretwisted blades subject to dynamic behavior constraints is studied. The restrictions on multiple blade natural frequencies and on maximum blade dynamic deflections are considered the dynamic behavior constraints. The aerodynamic forces acting on the rotating blades are simulated as harmonic excitations. Optimization techniques of the optimality‐criterion method and the method of modified feasible directions have been successfully developed and applied to minimize the weight of rotating pretwisted blades. Based on these techniques, the numerical results show that the effect of setting angle on the optimal design weight for the first frequency‐constraint case is more significant than that for the second frequency‐constraint case. It is also shown that the changes of pretwist angle will considerably affect the optimal design weight for the second frequency‐constraint case. However the effect is not significant for the fundamental frequency‐constraint case. The results also indicate that the increase of rotating speed will decrease the optimal design weight.
publisherAmerican Society of Civil Engineers
titleOptimization of Rotating Blades with Dynamic‐Behavior Constraints
typeJournal Paper
journal volume4
journal issue2
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(1991)4:2(127)
treeJournal of Aerospace Engineering:;1991:;Volume ( 004 ):;issue: 002
contenttypeFulltext


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