Optimal Supersonic Air-Launching Rocket Design Using Multidisciplinary System Optimization Approach. - Jae-Woo Lee; Young Chang Choi; Yung-Hwan Byun (FSKD (1), 2005)

Optimal Space Launcher Design Using a Refined Response Surface Method. - Jae-Woo Lee; Kwon-Su Jeon; Yung-Hwan Byun; Sang-Jin Kim (FSKD (1), 2005)

Rotor Design for the Performance Optimization of Canard Rotor/Wing Aircraft. - Jae-Woo Lee; Kwon-Su Jeon; Min-Ji Kim; Yung-Hwan Byun; Chang J. Kim; Yung H. Yu (ICCSA (5), 2006)

Development of Requirement Driven Design Concept Selection Process in Aerospace System. - Hyeong-Uk Park; Mee-Young Park; Seung-Jin Lee 003; Jae-Woo Lee; Yung-Hwan Byun (ICCSA (5), 2006)

Development of Integrated Missile System Design Framework Using Distributed Computing Environment. - Seung-Jin Lee 003; Woohyun Kim; Jae-Woo Lee; Yung-Hwan Byun (ICCSA Workshops, 2007)

Preliminary Design of the Hybrid Air-launching Rocket for Nanosat. - Jae-Woo Lee; Kyung-Ho Noh; Yung-Hwan Byun; Bong-Kyo Park (ICCSA Workshops, 2007)

The repetitive optimization design strategy using neural network and hybrid algorithm. - Nhu-Van Nguyen; Kwon-Su Jeon; Jae-Woo Lee; Yung-Hwan Byun (RIVF, 2008)

Multidisciplinary Design Approach Using Repetitive Response Surface Enhancement and Global Optimization. - Kwon-Su Jeon; Jae-Woo Lee; Yung-Hwan Byun (SNPD, 2008)

Comprehensive aircraft configuration design tool for Integrated Product and Process Development. - Abdulaziz Azamatov; Jae-Woo Lee; Yung-Hwan Byun (Adv. Eng. Softw., 2011)