AERO2S computer code developed to aid design engineers in selection and evaluation of aerodynamically efficient wing/canard and wing/horizontal-tail configurations that includes simple hinged-flap systems. Code rapidly estimates longitudinal aerodynamic characteristics of conceptual airplane lifting-surface arrangements. Developed in FORTRAN V on CDC 6000 computer system, and ported to MS-DOS environment.
Computer Code Aids Design Of Wings
NASA Tech Briefs ; 17 , 3
1993-03-01
Sonstige
Keine Angabe
Englisch
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