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.
Transonic flow past swept wings
NASA Tech Briefs ; 4 , 4
1980-06-01
Miscellaneous
No indication
English
Study of transonic flow over swept wings
NTRS | 1983
Study of Transonic Flow over Swept Wings
NTIS | 1983