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- W324623603 abstract "Report presenting an investigation in the high-speed tunnel to determine the effects on the chordwise pressure and section force and moment coefficients near midspan of deflecting a flap-type control with an attached tab on a swept wing. The semispan 35 degree sweptback wing had an NACA 65A006 airfoil section, an aspect ratio of 4, and a taper ratio of 0.6." @default.
- W324623603 created "2016-06-24" @default.
- W324623603 date "1954-03-29" @default.
- W324623603 modified "2023-09-27" @default.
- W324623603 title "Chordwise pressures and section moment force and moment coefficients at high subsonic speeds near midspan of a tapered 35 degree sweptback wing with a flap-type control and an attached tab" @default.
- W324623603 hasPublicationYear "1954" @default.
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