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- W327402331 abstract "Report presenting an investigation by the transonic-bump method through a range of Mach numbers in the high speed 7- by 10-foot tunnel to determine the lateral-control characteristics of a semispan wing-fuselage combination equipped with flap-type and spoiler-type controls. Both the flap-type and spoiler-type controls provide lateral control through the Mach number range investigated." @default.
- W327402331 created "2016-06-24" @default.
- W327402331 creator A5070038259 @default.
- W327402331 date "1950-07-18" @default.
- W327402331 modified "2023-09-27" @default.
- W327402331 title "Lateral-control investigation of flap-type and spoiler-type controls on a wing with quarter-chord-line sweepback of 60 degrees, aspect ratio 2, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bump method" @default.
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