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美国政府科技报告
>Aerodynamic Characteristics in the Approach, Superfine and Negative Pitch Ranges of Two Four-Bladed Propellers with N.A.C.A. Series 16 Blade Sections a Report of Tests carried out Jointly by the Technical Staffs of de Havilland Propellers, Limited, and Rotol, Limited.
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Aerodynamic Characteristics in the Approach, Superfine and Negative Pitch Ranges of Two Four-Bladed Propellers with N.A.C.A. Series 16 Blade Sections a Report of Tests carried out Jointly by the Technical Staffs of de Havilland Propellers, Limited, and Rotol, Limited.
Tests were conducted on two similar full-scale propellers in the 24-ft Wind Tunnel at the Royal Aircraft Establishment by representatives of Rotol, Ltd. and de Havilland Propellers, Ltd. to measure the aerodynamic characteristics over a blade-angle range of — 20 deg to + 40 deg, measured at the 0 . 7 radius, and over a range of advance ratio of 0.1 to 2.4.
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