TY - JOUR AB - In this study, dynamic mesh method is implemented on a real coded genetic algorithm to demonstrate gain in computational time as well as in higher performance for optimized parameters. Since the differences developed at each step in geometries of new members are not significant, therefore, it is possible to use dynamic mesh methods for new members. In this work, because the population members are obtained by modifying the pervious ones, each member is considered as one step of geometry‐change of a deforming body, for examples, a wing inflating, deflating or cambering. VL - 76 IS - 3 SN - 0002-2667 DO - 10.1108/00022660410536050 UR - https://doi.org/10.1108/00022660410536050 AU - Vatandaş Ergüven AU - Özkol İbrahim AU - Kaya Metin O. PY - 2004 Y1 - 2004/01/01 TI - Using the dynamic mesh method for genetically obtained wing structures T2 - Aircraft Engineering and Aerospace Technology PB - Emerald Group Publishing Limited SP - 314 EP - 319 Y2 - 2024/03/29 ER -