TY - JOUR
T1 - Using the dynamic mesh method for genetically obtained wing structures
AU - Vatandaş, Ergüven
AU - Ozkol, Ibrahim
AU - Kaya, Metin O.
PY - 2004
Y1 - 2004
N2 - 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.
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.
KW - Flight dynamics
KW - Meshes
KW - Optimization techniques
KW - Programming and algorithm theory
UR - http://www.scopus.com/inward/record.url?scp=2542577046&partnerID=8YFLogxK
U2 - 10.1108/00022660410536050
DO - 10.1108/00022660410536050
M3 - Article
AN - SCOPUS:2542577046
SN - 0002-2667
VL - 76
SP - 314
EP - 319
JO - Aircraft Engineering and Aerospace Technology
JF - Aircraft Engineering and Aerospace Technology
IS - 3
ER -