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1°­ ÀÎÆ®·Î °íÈ­Áú 9ºÐ ÷ºÎÆÄÀÏ
2°­ [1] Ç×°ø¿ªÇÐÀÇ ±âÃÊ 26ºÐ ÷ºÎÆÄÀÏ
3°­ [2-1] Ç×°ø¿ªÇÐÀÇ ±âº»°ø½Ä1 - º¤ÅÍ¿Í ¿¬»ê °íÈ­Áú 48ºÐ ÷ºÎÆÄÀÏ
4°­ [2-2] Ç×°ø¿ªÇÐÀÇ ±âº»°ø½Ä2 - À¯Ã¼¸ðµ¨, À¯µµ°úÁ¤ 26ºÐ ÷ºÎÆÄÀÏ
5°­ [2-3] Ç×°ø¿ªÇÐÀÇ ±âº»°ø½Ä3 - ¿¬¼Ó¹æÁ¤½Ä, ¿îµ¿·®¹æÁ¤½Ä, ¿¡³ÊÁö¹æÁ¤½Ä 64ºÐ ÷ºÎÆÄÀÏ
6°­ [2-4] Ç×°ø¿ªÇÐÀÇ ±âº»°ø½Ä4 - À¯¼±, °¢¼Óµµ, Circulation 58ºÐ ÷ºÎÆÄÀÏ
7°­ [3-1] ºñÁ¡¼º, ºñ¾ÐÃ༺ À¯Ã¼1 - º£¸£´©ÀÌ °ø½Ä °íÈ­Áú 42ºÐ ÷ºÎÆÄÀÏ
8°­ [3-2] ºñÁ¡¼º, ºñ¾ÐÃ༺ À¯Ã¼2 - Laplace's Equation(1) 61ºÐ ÷ºÎÆÄÀÏ
9°­ [3-2] ºñÁ¡¼º, ºñ¾ÐÃ༺ À¯Ã¼2 - Laplace's Equation(2) 47ºÐ
10°­ [3-2] ºñÁ¡¼º, ºñ¾ÐÃ༺ À¯Ã¼2 - Laplace's Equation(3) 34ºÐ
11°­ [3-2] ºñÁ¡¼º, ºñ¾ÐÃ༺ À¯Ã¼2 - Laplace's Equation(4) 56ºÐ
12°­ [3-3] ºñÁ¡¼º, ºñ¾ÐÃ༺ À¯Ã¼3 - Generation of Lift 73ºÐ ÷ºÎÆÄÀÏ
13°­ [4-1] 2Â÷¿ø ÀÍÇü ÁÖº¯ÀÇ ºñ¾ÐÃ༺ À¯µ¿1 - Airfoils 32ºÐ ÷ºÎÆÄÀÏ
14°­ [4-2] 2Â÷¿ø ÀÍÇü ÁÖº¯ÀÇ ºñ¾ÐÃ༺ À¯µ¿2 - Low-speed flow over Airfoils 69ºÐ ÷ºÎÆÄÀÏ
15°­ [4-3] 2Â÷¿ø ÀÍÇü ÁÖº¯ÀÇ ºñ¾ÐÃ༺ À¯µ¿ 3(1) - Classical Thin Airfoil 20ºÐ ÷ºÎÆÄÀÏ
16°­ [4-3] 2Â÷¿ø ÀÍÇü ÁÖº¯ÀÇ ºñ¾ÐÃ༺ À¯µ¿ 3(2) - ´ëĪµÈ Airfoils 75ºÐ
17°­ [5-1] À¯ÇÑÇÑ °íÁ¤ÀÍ ÁÖº¯ÀÇ ºñ¾ÐÃ༺ À¯µ¿1 - Introduction 16ºÐ ÷ºÎÆÄÀÏ
18°­ [5-2] À¯ÇÑÇÑ °íÁ¤ÀÍ ÁÖº¯ÀÇ ºñ¾ÐÃ༺ À¯µ¿ 2(1,2) - Prandtl's Classifal LLT(Ÿ¿øÇü) 57ºÐ ÷ºÎÆÄÀÏ
19°­ [5-2] À¯ÇÑÇÑ °íÁ¤ÀÍ ÁÖº¯ÀÇ À¯µ¿ 2(3) - Prandtl's Classifal LLT(ÀÓÀÇ) 28ºÐ
20°­ [5-3] À¯ÇÑÇÑ °íÁ¤ÀÍ ÁÖº¯ÀÇ À¯µ¿3 - Various Wings 58ºÐ ÷ºÎÆÄÀÏ
21°­ [6] 3Â÷¿ø ºñ¾ÐÃ༺ À¯µ¿ - Elementary 3D incompressible flows 42ºÐ ÷ºÎÆÄÀÏ
22°­ Summary 10ºÐ ÷ºÎÆÄÀÏ
23°­ ¹®Á¦Ç®ÀÌ 1°­. Ç×°ø¿ªÇÐÀÇ ±âÃÊ (Ch1) 45ºÐ ÷ºÎÆÄÀÏ
24°­ ¹®Á¦Ç®ÀÌ 2°­. Ç×°ø¿ªÇÐÀÇ ±âº»°ø½Ä (Ch2) 38ºÐ ÷ºÎÆÄÀÏ
25°­ ¹®Á¦Ç®ÀÌ 3°­. Ç×°ø¿ªÇÐÀÇ ±âº»°ø½Ä (Ch3) 59ºÐ ÷ºÎÆÄÀÏ
26°­ ¹®Á¦Ç®ÀÌ 3-1°­. Áß°£°í»ç º¸Ãæ (Ch1~3) 47ºÐ ÷ºÎÆÄÀÏ
27°­ ¹®Á¦Ç®ÀÌ 4°­. 2Â÷¿ø ÀÍÇü ÁÖº¯ÀÇ ºñ¾ÐÃ༺ À¯µ¿ (Ch4) 28ºÐ ÷ºÎÆÄÀÏ
28°­ ¹®Á¦Ç®ÀÌ 5°­. À¯ÇÑÇÑ °íÁ¤ÀÍ ÁÖº¯ÀÇ À¯µ¿ (Ch5) 28ºÐ ÷ºÎÆÄÀÏ
29°­ ¹®Á¦Ç®ÀÌ 6°­. °£´ÜÇÑ Ãß°¡ ¹®Ç× 18ºÐ ÷ºÎÆÄÀÏ