Maximization of the lift/drag ratio of airfoils with a turbulent boundary layer
DOI10.1007/BF02698197zbMath0918.76060OpenAlexW2094242180MaRDI QIDQ1289508
Publication date: 31 May 1999
Published in: Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf02698197
convex functionalangle-of-attack dependenceconditional extremumincompressible separationless high-Reynolds flow
Shear flows and turbulence (76F10) General aerodynamics and subsonic flows (76G25) Variational methods applied to problems in fluid mechanics (76M30) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)
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Cites Work
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- Airfoil optimization by the method of inverse boundary-value problems
- Variational inverse boundary value problems of aerodynamics for subsonic gas flow
- Design and Optimization of airfoils in non‐stalling incompressible flow with a prescribed range of the angle of attack
- Variational problems of gas dynamics of nonequilibrium and equilibrium flows
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