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美国政府科技报告
>The use of the rolled-up vortex concept for predicting wing-tail interference and comparison with experiment at Mach number of 1.62 for a series of missile configurations having tandem cruciform lifting surfaces
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The use of the rolled-up vortex concept for predicting wing-tail interference and comparison with experiment at Mach number of 1.62 for a series of missile configurations having tandem cruciform lifting surfaces