Haeseong Cho

发表

A Computational approach for vertical launch system by coupled CFD/CSD with hybrid particle level-set method

SangJoon Shin, Haeseong Cho, HyunShik Joo, 2017 .

Parallel computation for three-dimensional shell analysis of curved configuration based on domain decomposition method

Jun-young Kwak, SangJoon Shin, Seil Kim, 2018, J. Comput. Sci..

Three-dimensional fluid–structure interaction analysis of a flexible flapping wing under the simultaneous pitching and plunging motion

Namhun Lee, SangJoon Shin, Haeseong Cho, 2016 .

Anaysis of Elasto-plastic Deforming of Sturcture by Hydrodynamic Force Using Fluid Structure Interaction Method

SangJoon Shin, Younghun Lee, Haeseong Cho, 2016 .

Improved Finite Element Domain Decomposition Method Using Local and Mixed Lagrange Multipliers

Olivier A. Bauchau, SangJoon Shin, Haeseong Cho, 2013 .

Computational Algorithm for Nonlinear Large-scale/Multibody Structural Analysis Based on Co-rotational Formulation with FETI-local Method

Jack J. Yoh, SangJoon Shin, Younghun Lee, 2016 .

Design and analysis of the link mechanism for the flapping wing MAV using flexible multi-body dynamic analysis

Chongam Kim, Young-Hwan Kim, SangJoon Shin, 2017 .

Design and Analysis of the Link Mechanism in the Flapping Wing MAV Using Flexible Multi-Body Dynamic Analysis

Chongam Kim, Young-Hwan Kim, SangJoon Shin, 2016 .

Development of a coupled analysis regarding the rotor/dynamic components of a rotorcraft

SangJoon Shin, Jin-Seok Jang, Hanyeol Ryu, 2014 .

Development of Three-Dimensional Anisotropic Shell Analysis Based on Domain Decomposition Method for Space Vehicle Engine Nozzle

SangJoon Shin, Seil Kim, Haeseong Cho, 2016 .

Development of Nonlinear Structural Analysis Using Co-rotational Finite Elements with Improved Domain Decomposition Method

SangJoon Shin, Haeseong Cho, HyunShig Joo, 2017 .

Effect of flexibility on flapping wing characteristics in hover and forward flight

Namhun Lee, SangJoon Shin, Haeseong Cho, 2018, Computers & Fluids.

Helicopter Forward Flight Prediction using Geometrically Exact Beam Model and an Advanced Unsteady Aerodynamics

Kwanjung Yee, SangJoon Shin, WonJong Eun, 2013 .

Parametric non-intrusive model order reduction for flow-fields using unsupervised machine learning

Haeseong Cho, SiHun Lee, SangJoon Shin, 2021 .

Reduced-order modeling of nonlinear structural dynamical systems via element-wise stiffness evaluation procedure combined with hyper-reduction

Maenghyo Cho, Euiyoung Kim, Haeseong Cho, 2021, Computational Mechanics.

Nonlinear weighting process in ghost-cell immersed boundary methods for compressible flow

Soogab Lee, Vignesh Saravanan, Haeseong Cho, 2021, J. Comput. Phys..

Improved Computational Approach for 3-D Realistic Insect-like Flapping Wing using Co-rotational Finite Elements

Namhun Lee, Haeseong Cho, Seungsoo Lee, 2017 .

Elastoplastic and contact analysis based on consistent dynamic formulation of co-rotational planar elements

Haeseong Cho, HyunShig Joo, SangJoon Shin, 2017 .

Geometrically nonlinear dynamic formulation for three-dimensional co-rotational solid elements

Haeseong Cho, SangJoon Shin, Haedong Kim, 2018 .

Combined co-rotational beam/shell elements for fluid–structure interaction analysis of insect-like flapping wing

Namhun Lee, Haeseong Cho, Seungsoo Lee, 2019, Nonlinear Dynamics.

Advanced Structural Analysis Based on Reduced-Order Modeling for Gas Turbine Blade

Yongse Kim, Haeseong Cho, SangJoon Shin, 2018, AIAA Journal.