首页> 美国政府科技报告 >Cal/Avlabs Symposium Proceedings (3rd), 18-20 June 1969, Buffalo, New York. Aerodynamics of Rotary Wing and V/STOL Aircraft. Volume I. Rotor/Propeller Aerodynamics. Rotor Noise
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Cal/Avlabs Symposium Proceedings (3rd), 18-20 June 1969, Buffalo, New York. Aerodynamics of Rotary Wing and V/STOL Aircraft. Volume I. Rotor/Propeller Aerodynamics. Rotor Noise

机译:Cal / avlabs symposium proceedings(3rd),1969年6月18日至20日,纽约布法罗。旋翼和V / sTOL飞机的空气动力学。第一卷。转子/螺旋桨空气动力学。转子噪音

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Contents: A continuous vortex sheet representation of deformed wakes of hovering propellers; Propeller wake deformation due to instability of a trailing vortex sheet; Vortex field, tip vortex, and shock formation on a model propeller; An experimental investigation of an oscillating two-dimensional airfoil in reverse flow; Design of airfoils for rotors; A hover performance analysis combining the strip-momentum and prescribed wake theories; Helicopter rotor noise generation; The importance of vortex shedding effects on helicopter rotor noise with and without blade slap; Prediction methods and trends for helicopter rotor noise; and Rotor noise measurements in wind tunnels.

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