Airfoil design and optimization methods: recent progress at NLR

DOI<link itemprop=identifier href="https://doi.org/10.1002/(SICI)1097-0363(19990530)30:2<217::AID-FLD830>3.0.CO;2-6" /><217::AID-FLD830>3.0.CO;2-6 10.1002/(SICI)1097-0363(19990530)30:2<217::AID-FLD830>3.0.CO;2-6zbMath0922.76263OpenAlexW2012192630MaRDI QIDQ4247999

B. I. Soemarwoto, Th. E. Labrujere

Publication date: 18 October 1999

Full work available at URL: https://doi.org/10.1002/(sici)1097-0363(19990530)30:2<217::aid-fld830>3.0.co;2-6

zbMATH Keywords

Reynolds-averaged Navier-Stokes equationsEuler equationscost functionshape optimizationadjoint operator approachtwo-point drag-reduction design problem

Mathematics Subject Classification ID

Variational methods applied to problems in fluid mechanics (76M30) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Related Items (2)

Maximization of mass flow in a channel obstructed by an infinitely thin plate using a gradient-based control strategy ⋮ A new direct design method of wind turbine airfoils and wind tunnel experiment

Cites Work

• Aerodynamic design via control theory

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