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contributor authorBret Stanford
contributor authorPeter Ifju
date accessioned2017-05-08T21:16:25Z
date available2017-05-08T21:16:25Z
date copyrightApril 2009
date issued2009
identifier other%28asce%290893-1321%282009%2922%3A2%28173%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45158
description abstractMicro air vehicles are typically characterized by a low aspect ratio wing operating at low Reynolds numbers
publisherAmerican Society of Civil Engineers
titleMembrane Micro Air Vehicles with Adaptive Aerodynamic Twist: Numerical Modeling
typeJournal Paper
journal volume22
journal issue2
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2009)22:2(173)
treeJournal of Aerospace Engineering:;2009:;Volume ( 022 ):;issue: 002
contenttypeFulltext


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