NASA NTRS · 19930000092
Analyzing Transonic Flow Over A Wing And Fuselage
Abstract
TAWFIVE computer program calculates transonic flow over transport-type wing and fuselage. Combines multigrid acceleration technique in iterative solution of potential equation with use of integral-form boundary-layer equations to provide software tool computationally efficient, yet accurate enough for use in design. Simplifies solution process by breaking problem into loosely coupled set of modified equations. Inviscid-flow method, using standard inviscid-flow equations, valid in "outer" region away from wing, whereas boundary-layer equations valid in thin region near solid surface of wing. Written in FORTRAN 77.
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Melson, N. Duane, Streett, Craig L.. 1993-02-01. Analyzing Transonic Flow Over A Wing And Fuselage. https://ntrs.nasa.gov/citations/19930000092
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