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Browse "School of Mechanical and Aerospace Engineering(기계항공공학부)" by Subject fabricational thermal residual stress

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Showing results 1 to 5 of 5

1
(A) study on the smart cure method and joining method of the automotive co-cured hybrid aluminum/composite propeller shaft = 자동차용 동시경화 알루미늄/복합재료 동력전달축의 지능형 경화 방법 및 접합 공정에 관한 연구link

Kim, Hak-Sung; 김학성; et al, 한국과학기술원, 2006

2
Avoidance of fabricational thermal residual stresses in co-cure bonded metal-composite hybrid structures

Kim, Hak Sung; Lee, Dai Gil, JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, v.20, no.9, pp.959 - 979, 2006

3
Effect of the smart cure cycle on the performance of the co-cured aluminum/composite hybrid shaft

Kim, HS; Park, SW; Hwang, HY; Lee, Dai Gil, COMPOSITE STRUCTURES, v.75, no.1-4, pp.276 - 288, 2006-09

4
Reduction of fabricational thermal residual stress of the hybrid co-cured structure using a dielectrometry

Kim, HS; Lee, Dai Gil, COMPOSITES SCIENCE AND TECHNOLOGY, v.67, pp.29 - 44, 2007-01

5
Smart cure cycle with cooling and reheating for co-cure bonded steel/carbon epoxy composite hybrid structures for reducing thermal residual stress

Kim, Hak Sung; Park, Sang Wook; Lee, Dai Gil, COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, v.37, no.10, pp.1708 - 1721, 2006

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