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- W890505879 abstract "A 0.10-scale model of a swept-wing fighter airplane was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92 to determine the effects of adding underfuselage speed brakes. The results of brief spoiler-aileron lateral control tests also are included. The tests show acceptable trim and drag increments when the speed brakes are installed at the 32-71-inch fuselage station." @default.
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- W890505879 date "1959-01-01" @default.
- W890505879 modified "2023-09-27" @default.
- W890505879 title "An Experimental Investigation to Determine the Effect of Speed-Brake Position on the Longitudinal Stability and Trim of a Swept-Wing Fighter Airplane" @default.
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- W890505879 hasPublicationYear "1959" @default.
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