Numerical Calculation of Transonic Potential Flow about Wing-Body Combinations

DOI10.2514/3.61092zbMath0392.76047OpenAlexW2073784729MaRDI QIDQ4174417

David A. Caughey, Anthony Jameson

Publication date: 1979

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.61092

zbMATH Keywords

NumericalQuasilinearTransonicPotential FlowFinite-Difference GridStabilizedUpwind BiasWing-Body Combinations

Mathematics Subject Classification ID

Transonic flows (76H05) Supersonic flows (76J20) Software, source code, etc. for problems pertaining to fluid mechanics (76-04) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Numerical solution of discretized equations for boundary value problems involving PDEs (65N22)

Related Items (8)

Redesign of a supercritical wing in the presence of an engine nacelle ⋮ A combination conformal-transfinite mapping method for grids about fin- afterbody combinations ⋮ Algebraic grid generation for an afterbody with finite-span, tapered fins ⋮ Numerical results and stability analysis for the computation of the transonic flow problems using an artificial time formulation ⋮ Multi-grid calculation of three-dimensional transonic potential flows ⋮ Application of the multigrid method to calculations of transonic potential flow about wing-fuselage combinations ⋮ A multigrid algorithm for steady transonic potential flows around aerofoils using Newton iteration ⋮ Finite element methods for first-order hyperbolic systems with particular emphasis on the compressible Euler equations

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