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美国政府科技报告
>Hinge-moment and effectiveness characteristics of an aspect-ratio-8.2 flap-type control on a 60 degree delta wing at Mach numbers from 0.72 to 1.96
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Hinge-moment and effectiveness characteristics of an aspect-ratio-8.2 flap-type control on a 60 degree delta wing at Mach numbers from 0.72 to 1.96