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International Conference
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Total : 203, Now : 20 / 21 page
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13
Active Aeroelasticity in Rotary Wing Aircrafts- Author
- Shin, S.-J.
- Conference
- International Conference for Mechanical and Automotive Technologies 2005
- Period
- June 2005.
- Location
- Jeonju, Korea
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12
Computational Material Characterization of Active Fiber Composite- Author
- Yoon, T. H., Paik, S. H., Shin, S.-J., and Kim, S. J.
- Conference
- Proceedings of 15th International Conference on Adaptive Structures and Technologies
- Period
- October 25-27, 2004.
- Location
- Bar Habor, Maine
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11
Optimum Design Framework for Integrally Twisted Helicopter Blades- Author
- Cesnik, C. E. S., Mok, J., Parikh, A., and Shin, S.-J.
- Conference
- 45th AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
- Period
- April 19-22, 2004, AIAA Paper No. 2004-1761.
- Location
- Palm Springs, California
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10
Optimization Design Framework for Integrally Twisted Helicopter Blades- Author
- Carlos E. S. Cesnik, Jiwon Mok, Anish S. Parikh and SangJoon Shin
- Conference
- Optimization Design Framework for Integrally Twisted Helicopter Blades
- Period
- 19 - 22 April 2004
- Location
- Palm Springs, California
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9
Numerical Simulation of Actuation Behavior of Active Fiber Composites in Helicopter Rotor Blade Application- Author
- Paik, S. H., Kim, J. Y., Shin, S.-J. and Kim, S. J.
- Conference
- Proceeding of the 11th SPIE Annual International Symposium on Smart Structures and Materials
- Period
- March 15-18, 2004.
- Location
- San Diego, California
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8
NASA/Army/MIT Active Twist Rotor Closed-loop Control Test for Vibration Reduction- Author
- Shin, S.-J., Cesnik, C. E. S., and Hall, S. R.
- Conference
- Proceedings of the 29th European Rotorcraft Forum
- Period
- July, 2003.
- Location
- Friedrichshafen, Germany
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7
Closed-loop Control Test of the NASA/ Army/MIT Active Twist Rotor for Vibration Reduction- Author
- Shin, S.-J., Cesnik, C. E. S., and Hall, S. R.
- Conference
- Proceedings of the American Helicopter Society 59th Annual Forum
- Period
- May 6-8, 2003.
- Location
- Phoenix, Arizona
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6
Helicopter Performance and Vibration Enhancement by Twist-Actuated Blades- Author
- Shin, S.-J. and Cesnik, C. E. S.
- Conference
- 44th AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
- Period
- April 7-10, 2003, AIAA Paper No. 2003-1818.
- Location
- Norfolk, Virginia
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5
Control of Integrals Twist-Actuated Helicopter Blades for Vibrations Reduction- Author
- Shin, S.-J., Cesnik, C. E. S., and Hall, S. R.
- Conference
- Proceedings of the American Helicopter Society 58th Annual Forum
- Period
- June 11-13, 2002.
- Location
- Montreal, Canada
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4
Helicopter Vibration Reduction in Forward Flight Response Using Blade Integral Twist Control- Author
- Shin, S.-J. and Cesnik, C. E. S.
- Conference
- 43rd AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
- Period
- April 22-25, 2002, AIAA Paper No. 2002-1447.
- Location
- Denver, Colorado
Seoul National University Active Aeroelasticity and Rotorcraft Laboratory
School of Mechanical and Aerospace Engineering, Seoul National University,301-1357, 302-213-1, San 56-1, Shillim-Dong, Kwanak-Gu, Seoul, Korea (ROK)
301-1357 Tel : +82-2-880-1901(1901) / 302-213-1 Tel: +82-2-880-1608(1608)
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