Th01D
Session 5A Àü»ê¿ªÇÐ I
ÁÂÀå : À̵ÎÈ£ 15:00~16:30
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Th01D-1
A reliability-based framework for fatigue damage prognosis of composite aircraft tail wing structure
KHALID SALMAN, Yeong Rim Noh, Heung Soo Kim(µ¿±¹´ëÇб³ ±â°è°øÇаú)
Th01D-2
°í¿ë·® Àü±Ø°³¹ßÀ» À§ÇÑ Si-³ª³ë¿ÍÀÌ¾î ¹è¿­ÀÇ Àü±âÈ­ÇÐ-·¹º§¼Â ÃÖÀû¼³°è Design Optimization of Silicone Nanowire Arrangement by the Electrochemical Level-set Method
³²»ó¼ö, ¹Ú°æ¹Î, ±èö(°æºÏ´ëÇб³)
Th01D-3
MPI¸¦ È°¿ëÇÑ Àç·áÀÔÀÚ¹ýÀÇ ÀÔÀÚ±â¹Ý º´·ÄÈ­ ±â¹ý °³¹ß
±¸Å¹È¸(¼­¿ï°úÇбâ¼ú´ëÇб³ ÀϹݴëÇпø), ±èÇö±Ô(¼­¿ï°úÇбâ¼ú´ëÇб³)
Th01D-4
´ÙÁ߱׸®µå Æ丮´ÙÀ̳ª¹Í Çؼ®¹ý°ú ´ÙÁß·¹º§ ¼Õ»ó ¸ÅÇÎÀ» ÅëÇÑ ÁØÁ¤Àû ±Õ¿­ ÀüÆÄ Çؼ® ±â¹ý ¿¬±¸
ÇÏÀ±µµ(±º»ê´ëÇб³ °ø°ú´ëÇÐ), Á¶±¤Çö(±º»ê´ëÇб³ ÀÚ¿¬´ëÇÐ)
Th01D-5
Total Lagrangian ±â¹Ý À½ÇØÀû ÀÔÀÚ¹ýÀ» ÀÌ¿ëÇÑ ¿ÜÆȺ¸ µ¿Àû °Åµ¿ Çؼ®
À̿ϱâ, º¯Á¦À±, ÁÖ¿µ¼®(ÀÌ¿¡ÀÌÆ® ÁÖ½Äȸ»ç)
Th01D-6
±ËµµÂ÷·®ÀÇ µ¿Æ¯¼º ºÐ¼®À» À§ÇÑ 2Â÷¿ø ¸ðµ¨ °³¹ß
Á¤»ç¹«¿¤, ÀÌÁ¾¼®, ¿ÀÀçÀÌ(ÇÑÈ­µðÆ潺)
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