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美国政府科技报告
>An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degrees sweepback : estimated downwash angles derived from pressure measurements on the tail at Mach numbers of 1.40 and 1.59
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An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degrees sweepback : estimated downwash angles derived from pressure measurements on the tail at Mach numbers of 1.40 and 1.59