An Investigation of the Vibratory and Acoustic Benefits Obtainable by the Elimination of the Blade Tip Vortex

By White Richard P.  

Journal of the American Helicopter Society, Vol. 18, Iss. 4, 1973-10 ,pp. : 35-44

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Influence of Tip Shape, Chord, Blade Number, and Airfoil on Advanced Rotor Performance

By McVeigh Michael A.   McHugh Francis J.  

Journal of the American Helicopter Society, Vol. 29, Iss. 4, 1984-10 ,pp. : 55-62

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Research on Model Helicopter Rotor Blade Slap at Moderate Tip Speeds

By Leighton Kenneth P.  

Journal of the American Helicopter Society, Vol. 27, Iss. 3, 1982-07 ,pp. : 11-17

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Model- to Full-Scale Comparisons of Helicopter Blade-Vortex Interaction Noise

By Schmitz F. H.   Boxwell D. A.   Le´wy S.   Dahan C.  

Journal of the American Helicopter Society, Vol. 29, Iss. 2, 1984-04 ,pp. : 16-25

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Blade-Vortex Interaction Acoustic Results from a Forty Percent Model Rotor in the DNW

By Martin Ruth M.   Splettstoesser Wolf R.  

Journal of the American Helicopter Society, Vol. 33, Iss. 1, 1988-01 ,pp. : 37-46

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