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美国政府科技报告
>Some effects of aeroelasticity and sweepback on the rolling effectiveness and drag of a 1/11-scale model of the Bell X-5 airplane wing at Mach numbers from 0.6 to 1.5
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Some effects of aeroelasticity and sweepback on the rolling effectiveness and drag of a 1/11-scale model of the Bell X-5 airplane wing at Mach numbers from 0.6 to 1.5