AERODYNAMIC ANALYSIS OF HELICOPTER SHROUDED TAIL ROTOR BY MOMENTUM THEORYOA
In this paper, in order to clarify the gains of the shroud in the shrouded tail rotor system, a thrust division factor q , which represents the ratio of the shroud thrust to the total thrust of the shrouded tail rotor, is …查看全部>>
徐国华;王适存
南京航空航天大学直升机技术研究所南京航空航天大学直升机技术研究所
helicopters tail rotors shroud aerodynamic analysis
《南京航空航天大学学报：英文版》 1998 (2)
P.50-54,5
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