| Vibratory loads reduction testing of the NASA/Army/MIT active twist rotor ML Wilbur, PH Mirick, WT Yeager, CW Langston, CES Cesnik, SJ Shin Journal of the American Helicopter Society 47 (2), 123-133, 2002 | 127 | 2002 |
| Dynamic response of active twist rotor blades CES Cesnik, SJ Shin, ML Wilbur Smart materials and structures 10 (1), 62, 2001 | 96 | 2001 |
| Aeroservoelastic and structural dynamics research on smart structures conducted at NASA Langley Research Center AMR McGowan, WK Wilkie, RW Moses, RC Lake, JL Pinkerton-Florance, ... Smart Structures and Materials 1998: Industrial and Commercial Applications …, 1998 | 57 | 1998 |
| Acoustic Aspects of Active‐Twist Rotor Control ER Booth, ML Wilbur Journal of the American Helicopter Society 49 (1), 3-10, 2004 | 56 | 2004 |
| Modeling, Design, and Testing of the NASA/ARMY/MIT Active Twist Rotor Prototype Blade CES Cesnik, S Shin, WK Wilkie, ML Wilbur, PH Mirick AHS International Annual Forum, 55 th, Montreal, Canada, 533-544, 1999 | 42 | 1999 |
| Technical Notes: Reduction of Blade‐Vortex Interaction Noise Through Higher Harmonic Pitch Control TF Brooks, ER Booth, JR Jolly, WT Yeager, ML Wilbur Journal of the American Helicopter Society 35 (1), 86-91, 1990 | 40 | 1990 |
| Aeroelastic analysis of the NASA/Army WK Wilkie, ML Wilbur, PH Mirick, CES Cesnik, SJ Shin MIT active twist rotor. In American Helicopter Society 55th Forum, Montreal …, 1999 | 38 | 1999 |
| Aerodynamic design study of an advanced active twist rotor MK Sekula, ML Wilbur, WT Yeager Jr AHS 4th Decennial Specialists''Conference on Aeromechanics, 2003 | 33 | 2003 |
| Further examination of the vibratory loads reduction results from the NASA/Army/MIT active twist rotor test ML Wilbur, WT Yeager Jr, MK Sekula 58th American Helicopter Society Annual Forum, 2002 | 33 | 2002 |
| Vibratory loads reduction testing of the NASA/ARMY/MIT Active Twist Rotor ML Wilbur, PH Mirick, WT Yeager Jr, CW Langston, CES Cesnik, SJ Shin | 32 | 2001 |
| Hover testing of the NASA/ARMY/MIT active twist rotor prototype blade ML Wilbur, WT Yeager Jr, WK Wilkie, CES Cesnik, SJ Shin | 32 | 2000 |
| Design and manufacturing of a model-scale active twist rotor prototype blade SJ Shin, CES Cesnik, WK Wilkie, ML Wilbur Journal of Intelligent Material Systems and Structures 19 (12), 1443-1456, 2008 | 30 | 2008 |
| Active-twist rotor control applications for UAVs ML Wilbur, WK Wilkie Transformational Science And Technology For The Current And Future Force …, 2006 | 30 | 2006 |
| Hover testing of the NASA/ARMY ML Wilbur, WT Yeager Jr, WK Wilkie, CES Cesnik, S Shin MIT active twist rotor prototype blade, 2000 | 28 | 2000 |
| Aeroelastic analysis of the NASA/Army/MIT active twist rotor WK Wilkie, ML Wilbur, PH Mirick, CES Cesnik, S Shin American Helicopter Society 55th Annual Forum, 1999 | 28 | 1999 |
| Modeling, design and testing of the NASA/ARMY CES Cesnik, SJ Shin, WK Wilkie, ML Wilbur, PH Mirick MIT active twist rotor prototype blade. In 55th American Helicopter Society …, 1999 | 26 | 1999 |
| Further examination of the vibratory loads reduction results from the NASA/ARMY ML Wilbur, WT Yeager Jr, MK Sekula MIT active twist rotor test, 2002 | 24 | 2002 |
| Wind-tunnel evaluation of an advanced main-rotor blade design for a utility-class helicopter WT Yeager Jr, WR Mantay, ML Wilbur, RG Cramer Jr, JD Singleton | 24 | 1987 |
| A demonstration of passive blade twist control using extension-twistcoupling R LAKE, M NIXON, M WILBUR, J SINGLETON, P MIRICK 33rd Structures, Structural Dynamics and Materials Conference, 2468, 1992 | 22 | 1992 |
| The effect of tip geometry on active-twist rotor response ML Wilbur, MK Sekula American Helicopter Sociert 61st Annual Forum, 2005 | 20 | 2005 |
