Upper Estimates of Airfoil Aerodynamic Characteristics for a Viscous Incompressible Flow

DOI<link itemprop=identifier href="https://doi.org/10.1002/(SICI)1521-4001(199911)79:11<757::AID-ZAMM757>3.0.CO;2-V" /><757::AID-ZAMM757>3.0.CO;2-V 10.1002/(SICI)1521-4001(199911)79:11<757::AID-ZAMM757>3.0.CO;2-VzbMath0960.76026OpenAlexW2051945081MaRDI QIDQ3835821

A. M. Elizarov, D. A. Fokin

Publication date: 9 April 2000

Full work available at URL: https://doi.org/10.1002/(sici)1521-4001(199911)79:11<757::aid-zamm757>3.0.co;2-v

zbMATH Keywords

lift coefficientangle of attackHölder continuous functionshigh Reynolds numberupper estimatesincompressible viscous flowsharp trailing edgeaerodynamic ratioairfoil shape optimizationinverse boundary value methodminimization of convex functionalsnon-separating turbulent boundary layer

Mathematics Subject Classification ID

Variational methods applied to problems in fluid mechanics (76M30) Turbulent boundary layers (76F40) Flow control and optimization for incompressible viscous fluids (76D55)

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