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Performance evaluation of two meta-heuristic schemes in airfoil design

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Publication:1639455
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DOI10.1007/s13369-016-2102-xzbMath1391.76565OpenAlexW2334191587MaRDI QIDQ1639455

J. Srinivas, L. Prabhu

Publication date: 12 June 2018

Published in: Arabian Journal for Science and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s13369-016-2102-x


zbMATH Keywords

surrogate modelmicro-genetic algorithmairfoil parametersmicro-differential evolutionsubsonic incompressible flow


Mathematics Subject Classification ID

Lua error in Module:PublicationMSCList at line 37: attempt to index local 'msc_result' (a nil value).



Uses Software

  • FlowLab


Cites Work

  • Bézier-PARSEC: an optimized aerofoil parameterization for design
  • Aerodynamic optimization via multi-objective micro-genetic algorithm with range adaptation, knowledge-based reinitialization, crowding and \(\varepsilon \)-dominance
  • Some models of viscous–inviscid interaction
  • Unnamed Item
  • Unnamed Item


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