Kuo-An Yuan

发表

SI'KI-CTCR AI, OPTI\II7,ATIOX OF COJIPOSITE HEIJCOPTER ROTOR BI,AIILS WITH SWEPT nPs FOR VIBRATIOS REDUCTIOS n- FORWARD FIKHT

Kuo-An Yuan, Pcretz P. Friedmanni, K. Yuan, 1994 .

Correlation studies for hingeless rotors in forward flight

Peretz P. Friedmann, Kuo-An Yuan, Comandur Venkatesan, 1994 .

A new aeroelastic model for composite rotor blades with straight and swept tips

Peretz P. Friedmann, Kuo-An Yuan, Comandur Venkatesan, 1992 .

Calculation of Corrections to Linear Aerodynamic Methods for Static and Dynamic Analysis and Design

Kuo-An Yuan, Myles L. Baker, Patrick J. Goggin, 1998 .

Technical Note: Correlation Studies for Hingeless Rotors in Forward Flight Using 2GCHAS

Peretz P. Friedmann, Kuo-An Yuan, Thomas A. Millott, 1998 .

Structural Optimization for Vibration Reduction of Composite Helicopter Rotor Blades with Advanced Geometry Tips Subject to Multidisciplinary Constraints

Peretz P. Friedmann, Kuo-An Yuan, Los Angeles, 1995 .

Aeroelastic modeling of composite rotor blades with straight and swept tips

Peretz P. Friedmann, Kuo-An Yuan, Comandur Venkatesan, 1992 .

Structural optimization of composite helicopter rotor blades with swept tips for vibration reduction in forward flight

Kuo-An Yuan, Peretz Friedmann, P. Friedmann, 1994 .