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- W284862009 abstract "Memorandum presenting an investigation conducted in the high-speed 7- by 10-foot tunnel of the effects of various horizontal fuselage forebody fins on the directional and longitudinal stability characteristics at high subsonic speeds of a complete model with a 45 degree sweptback wing mounted in a high position on the fuselage. The model wing had an aspect ratio of 4, a taper ratio of 0.30, and NACA 65A006 airfoil sections parallel to the free stream." @default.
- W284862009 created "2016-06-24" @default.
- W284862009 creator A5047762320 @default.
- W284862009 date "1957-01-16" @default.
- W284862009 modified "2023-09-27" @default.
- W284862009 title "Investigation at high subsonic speeds of the effects of various horizontal fuselage forebody fins on the directional and longitudinal stability of a complete model having a 45 degree sweptback wing" @default.
- W284862009 hasPublicationYear "1957" @default.
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