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Investigation Of A Slotted Rotorcraft Airfoil At Mach Numbers From 0.20 To 0.88 At Full-Scale Reynolds Numbers

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Investigation Of A Slotted Rotorcraft Airfoil At Mach Numbers From 0.20 To 0.88 At Full-Scale Reynolds Numbers

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  • SKU # : sm_aeromech_1994_029_Noonan

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Investigation Of A Slotted Rotorcraft Airfoil At Mach Numbers From 0.20 To 0.88 At Full-Scale Reynolds Numbers

Authors / Details: Kevin W. Noonan, Dennis O. Allison, and Sharon Stanaway, NASA

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