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- W390855983 abstract "Report presenting the first results of pressure measurements obtained on a fuselage and a 45 degree sweptback wing-fuselage combination at transonic speeds in the slotted test section of the 8-foot high-speed tunnel. The test was part of a systematic investigation of varying amounts of sweepback on wings suitable for transonic flight. Results regarding the wing, fuselage, and fuselage with wing are provided." @default.
- W390855983 created "2016-06-24" @default.
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- W390855983 date "1951-09-14" @default.
- W390855983 modified "2023-09-27" @default.
- W390855983 title "Basic pressure measurements on a fuselage and a 45 degrees sweptback wing-fuselage combination at transonic speeds in the slotted test section of the Langley 8-foot high-speed tunnel" @default.
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