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Propulsor Related Research at DLR - CROR Blade Optimization … · 2020. 6. 12. · 1.2 1.4 1.6 1.8 2 2.2 x [m] r a d u s [m 0 0.5 1 1.5 0.8 1 1.2 1.4 1.6 1.8 2 2.2 Pre sur 35 0 3
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