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Flow field around asymmetric flapping flat plate optimized using micro genetic algorithm
a Bandung Institute of Technology, Bandung, 40132, Indonesia
[vc_row][vc_column][vc_row_inner][vc_column_inner][vc_separator css=”.vc_custom_1624529070653{padding-top: 30px !important;padding-bottom: 30px !important;}”][/vc_column_inner][/vc_row_inner][vc_row_inner layout=”boxed”][vc_column_inner width=”3/4″ css=”.vc_custom_1624695412187{border-right-width: 1px !important;border-right-color: #dddddd !important;border-right-style: solid !important;border-radius: 1px !important;}”][vc_empty_space][megatron_heading title=”Abstract” size=”size-sm” text_align=”text-left”][vc_column_text]© 2015 American Institute of Aeronautics and Astronautics Inc. All rights reserved.Asymmetric flapping flight motion employs inclined stroke plane to support the hoverers weight by taking advantage of the drag force. The strategy reduces the energy cost of hoverer and thus the optimal motion of this asymmetric flapping motion is an interesting subject to be studied. To reveal this optimal motion, a heuristic optimization method based on micro genetic algorithm coupled with experiment to calculate fitness function was used to optimize the drag force of flapping flat plate with constraint on profile power. Particle flow visualization method is employed on the final optimal solution to reveal the flow field and to discover the important fluid phenomenon. Result shows that the attachment of large leading edge vortex to the plate is essential to maintain high force production during downstroke phase. Interaction of flow field from previous stroke and current stroke also creates an advantage to enhance force production in upstroke phase. Basic philosophy of typical asymmetric hovering flapping motion is also discovered in the optimal solution where the downstroke acts as primary force generator whereas the upstroke serves as a motion to return the wing to its original position and only produces small amount of drag force with small profile power.[/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”Author keywords” size=”size-sm” text_align=”text-left”][vc_column_text]Fitness functions,Flapping flat plates,Fluid phenomenon,Heuristic optimization method,Leading-edge vortices,Micro genetic algorithm,Optimal solutions,Visualization method[/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”Indexed keywords” size=”size-sm” text_align=”text-left”][vc_column_text][/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”Funding details” size=”size-sm” text_align=”text-left”][vc_column_text][/vc_column_text][vc_empty_space][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][vc_empty_space][megatron_heading title=”DOI” size=”size-sm” text_align=”text-left”][vc_column_text]https://doi.org/10.2514/6.2014-0745[/vc_column_text][/vc_column_inner][vc_column_inner width=”1/4″][vc_column_text]Widget Plumx[/vc_column_text][/vc_column_inner][/vc_row_inner][/vc_column][/vc_row][vc_row][vc_column][vc_separator css=”.vc_custom_1624528584150{padding-top: 25px !important;padding-bottom: 25px !important;}”][/vc_column][/vc_row]