NASA NTRS · 19790000542
Transonic flow past swept wings
Abstract
FLO-22 computer program aids in numerical analysis of transonic potential flow past lifting, swept wing. FLO-22 uses relaxation method to solve finite-difference approximation of full-potential equation for transonic flow past configuration consisting of wing or arbitrary planform and dihedral extending from symmetry plane or wall. Comparisons of FLO-22 calculated results with experimental data for both conventional and super-critical transport wings show good agreement.
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Caughey, D. A., Jameson, A.. 1980-06-01. Transonic flow past swept wings. https://ntrs.nasa.gov/citations/19790000542
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