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美国政府科技报告
>Longitudinal and lateral stability and control characteristics at Mach number 2.01 of a 60 degree delta-wing airplane configuration equipped with a canard control and with wing trailing-edge flap controls
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Longitudinal and lateral stability and control characteristics at Mach number 2.01 of a 60 degree delta-wing airplane configuration equipped with a canard control and with wing trailing-edge flap controls