Hybrid numerical technique for evaluating wing aerodynamic loading with propeller interference

DOI10.1016/S0045-7930(98)00055-3zbMath0958.76053OpenAlexW2046295086MaRDI QIDQ1962730

Yanyan Li

Publication date: 31 January 2000

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7930(98)00055-3

zbMATH Keywords

boundary element methodfree wake analysismodified wing loadspropeller interferencetime-averaged aerodynamic characteristics

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Boundary element methods applied to problems in fluid mechanics (76M15)

Cites Work

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• Helmholtz decomposition revisited: Vorticity generation and trailing edge condition. I. Incompressible flows
• Vector Green's function method for unsteady Navier-Stokes equations
• Numerical solution of steady Navier-Stokes problems using integral representations
• On an extension of Prandti's lifting line theory to curved wings
• Boundary element method for the analysis of the unsteady flow aroundextreme propeller geometries
• Effect of airfoil (trailing-edge) thickness on the numerical solution of panel methods based on the Dirichlet boundary condition
• Nonlinear steady incompressible lifting-surface analysis with wake roll-up
• Explicit Kutta Condition for Unsteady Two-Dimensional High-Order Potential Boundary Element Method
• Subsonic Potential Aerodynamics for Complex Configurations : A General Theory

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