Open Access



构型 弹翼上的阻力/N 弹翼上的侧向力/N 突起物产生的阻力/N
L5, 5 12.22 -7.21 5.87
L10, 5 11.92 -8.41 5.85
L15, 5 11.98 -9.01 6.13

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