03# 04; 00; 01 02 - . begin end aerodrag_element bearing1 bearing2 fix0 fix1 relative base timoschenko_input c2_def hawc_dll matlab_link mann newmark TOWER_SHADOW_POTENTIAL main_body relative aerodrag constraint orientation simulation new_htc_structure dll wind aero output begin end 00 01 02 03 04 05 06 07 08 09 10 11 12 13 14 15 16 17 18 19 20 21 22 23