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International Conference
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Total : 198, Now : 9 / 20 page
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118
Parametric study of the vertical launcher by coupled CFD/CSD with hybrid particle level-set method- Author
- H. S. Joo., H. S. Cho., Y. H. Lee., M. C. Gwak., S-J. Shin., and J. I. Yoh
- Conference
- Coupled Problem 2017
- Period
- 2017.06.12-2017.06.14
- Location
- Rhodes Island, Greece
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117
Implicit fluid-structure interaction analysis using realistic structural modeling for insect-like flapping wing- Author
- H. S. Cho., N. Lee., S-J. Shin., and, S. Lee
- Conference
- Coupled Problem 2017
- Period
- 2017.06.12-2017.06.14
- Location
- Rhodes Island, Greece
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116
Advancement of the SNUF Blade Design through Flap Configuration Parametric Study and Optimization Framework- Author
- Eun, W. J., Sim, J. S., Lee, S. W. and Shin, S. J.
- Conference
- 73rd American Helicopter Society International Annual Forum,
- Period
- May 8-11, 2017
- Location
- Fort Worth, TX, USA.
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115
Improved Computational Approach for 3-D Realistic Insect-like Flapping Wing using Co-rotational Finite Element- Author
- H. S. Cho, N. H. Lee, S.-J. Shin, S. S. Lee., and S. Y. Kim
- Conference
- AIAA Scteich 2017
- Period
- 9 - 13 January 2017
- Location
- Grapevine, Texas, USA
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114
A Computational approach for vertical launch system by coupled CFD/CSD with hybrid particle level-set method- Author
- H. S. Joo, H. S. Cho., and S.-J. Shin
- Conference
- AIAA Scitech 2017
- Period
- 9 - 13 January 2017
- Location
- Grapevine, Texas, USA
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113
Development of Three-dimensional Structural Analysis for Engine Nozzle Using Anisotropic Facet Shell Element- Author
- S. I. Kim, H. S. Cho, H. S. Joo., and S.-J. Shin
- Conference
- AIAA Scitech 2017
- Period
- 9 - 13 January 2017
- Location
- Grapevine, Texas, USA
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112
Development of Three-Dimensional Anisotropic Shell Analysis Based on Domain Decomposition method for Space Vehicle Engine Nozzle- Author
- Joo, H. S., Cho, H S., Kim, S. I., and S.-J. Shin
- Conference
- International Conference for Computational Methods
- Period
- 1-4 August 2016
- Location
- Berkeley, USA
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111
Further Parametric Study using Rotor Structural Design Optimization Framework for Compound Rotorcraft with Lift Offset- Author
- Sim. J., Kang. Y., Eun. W., Lim. J., Shin. S.
- Conference
- 2016 AHS Technical Meeting on Aeromechanics Design for Vertical Lift
- Period
- Jan 20-22, 2016.
- Location
- San Francisco, California, USA
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110
Transient Flow Analysis and Static Bench Measurements for an Active Trailing-Edge Flap- Author
- Visconti. U., Kang. J., Lim. J. Sim. J., Shin. S.
- Conference
- 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
- Period
- Jan 4-8, 2016.
- Location
- San Diego, California, USA
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109
Design and Analysis of the Link Mechanism in the Flapping Wing MAV Using Flexible Multi-Body Dynamic Analysis- Author
- Jeon. J., Cho. H., Kim. Y., Lee. J., Shin. S., Kim. C., and Kim, S.
- Conference
- 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
- Period
- Jan 4-8, 2016.
- Location
- San Diego, California, USA
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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