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美国政府科技报告
>Experimental investigation at high subsonic speeds of the rolling stability derivatives of a complete model with an aspect-ratio-2.52 wing having an unswept 72-percent-chord line and a high horizontal tail
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Experimental investigation at high subsonic speeds of the rolling stability derivatives of a complete model with an aspect-ratio-2.52 wing having an unswept 72-percent-chord line and a high horizontal tail