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- W212251067 abstract "Report presenting a low-speed investigation to determine the lateral static and rotary derivatives of a model of a high-speed fighter airplane. The purpose was to compare experimental stability derivatives with derivatives estimated for a wing-fuselage combination, a vertical- and horizontal-tail combination, and a complete model." @default.
- W212251067 created "2016-06-24" @default.
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- W212251067 date "1954-01-11" @default.
- W212251067 modified "2023-09-27" @default.
- W212251067 title "Measured and Estimated Lateral Static and Rotary Derivatives of a 1/12-scale Model of a High-speed Fighter Airplane with Unswept Wings" @default.
- W212251067 hasPublicationYear "1954" @default.
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