Optimization design study of low-Reynolds-number high-lift airfoils for the high-efficiency propeller of low-dynamic vehicles in stratosphere

DOI10.1007/S11431-010-4087-0zbMath1269.76098OpenAlexW2078350459MaRDI QIDQ2393390

Peiqing Liu, Bowen Zhong, Rong Ma

Publication date: 7 August 2013

Published in: Science China. Technological Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-010-4087-0

zbMATH Keywords

multi-objective optimizationEXTREMhierarchical multi-objective optimizationlow Reynolds number airfoil

Mathematics Subject Classification ID

Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (2)

Airfoil optimization design based on the pivot element weighting iterative method ⋮ Aerodynamic design optimization of transonic natural-laminar-flow airfoil at low Reynolds number

Uses Software

• XFOIL

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