SUBAERF2 program developed to provide for analysis of subsonic aerodynamics and design by iteration of low-speed wing/flap systems. Based on linearized-theory lifting-surface solution but also accounts for some nonlinear characteristics. Effects of leading- and trailing-edge flaps included. New and improved version of programs described in LAR-13116 and LAR-12987, and replaces both of them. Written in FORTRAN V.
Code For Analysis Of Wing-And-Flap Systems
NASA Tech Briefs ; 14 , 10
1990-10-01
Miscellaneous
No indication
English
Flap support assembly for wing comprising flap and wing comprising flap
European Patent Office | 2023
|Aerodynamic Analysis of Low-Speed Wing-Flap Systems
NTRS | 1985
|