Investigation of flap-type ailerons on an untapered wing having an aspect ratio of 3.7, 45 degree sweepback, and an NACA 65A009 airfoil section : transonic-bump method
23.08.1950
Sonstige
Keine Angabe
Englisch
Flow about section of finite-aspect-ratio NACA-0018 airfoil on transonic bump
Engineering Index Backfile | 1953
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