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- W212933883 abstract "The results of transonic flight measurements of the longitudinal stability characteristics of the Douglas D-558-II research airplane in the original configuration and with outboard fences mounted on the wings are presented. The levels of normal-force coefficient at which the stability decreases and pitch-up starts have been determined for both airplane configurations at Mach numbers up to about 0.94." @default.
- W212933883 created "2016-06-24" @default.
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- W212933883 date "1953-03-13" @default.
- W212933883 modified "2023-09-27" @default.
- W212933883 title "Flight Determination of the Longitudinal Stability in Accelerated Maneuvers at Transonic Speeds for the Douglas D-558-II Research Airplane Including the Effects of an Outboard Wing Fence" @default.
- W212933883 hasPublicationYear "1953" @default.
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