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美国政府科技报告
>Flight investigation of the effect of a propulsive jet positioned according to the transonic area rule on the drag coefficients of a single-engine delta-wing configuration at Mach numbers from 0.83 to 1.36
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Flight investigation of the effect of a propulsive jet positioned according to the transonic area rule on the drag coefficients of a single-engine delta-wing configuration at Mach numbers from 0.83 to 1.36