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Steady state aerodynamic analysis of aeroplane wings with constant and varying cross section

Steady state aerodynamic analysis of aeroplane wings with constant and varying cross section

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Inspec keywords: subsonic flow; computational fluid dynamics; aircraft; lattice theory; mechanical engineering computing; aerodynamics; vortices; drag; FORTRAN; aerospace components; aerospace engineering

Subjects: Turbulent flows, convection, and heat transfer; Fluid mechanics and aerodynamics (mechanical engineering); Applied fluid mechanics; General fluid dynamics theory, simulation and other computational methods; Mechanical engineering applications of IT; Civil and mechanical engineering computing; General subsonic flows; Mechanical components; Aerospace engineering computing; Rotational flow, vortices, buoyancy and other flows involving body forces; Aerospace industry

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