Optimization of structures with multiple frequency constraints

1985 ◽  
Vol 20 (5) ◽  
pp. 869-876 ◽  
Author(s):  
N.S. Khot
2021 ◽  
pp. 136943322110262
Author(s):  
Mohammad H Makiabadi ◽  
Mahmoud R Maheri

An enhanced symbiotic organisms search (ESOS) algorithm is developed and presented. Modifications to the basic symbiotic organisms search algorithm are carried out in all three phases of the algorithm with the aim of balancing the exploitation and exploration capabilities of the algorithm. To verify validity and capability of the ESOS algorithm in solving general optimization problems, the CEC2014 set of 22 benchmark functions is first optimized and the results are compared with other metaheuristic algorithms. The ESOS algorithm is then used to optimize the sizing and shape of five benchmark trusses with multiple frequency constraints. The best (minimum) mass, mean mass, standard deviation of the mass, total number of function evaluations, and the values of frequency constraints are then compared with those of a number of other metaheuristic solutions available in the literature. It is shown that the proposed ESOS algorithm is generally more efficient in optimizing the shape and sizing of trusses with dynamic frequency constraints compared to other reported metaheuristic algorithms, including the basic symbiotic organisms search and its other recently proposed improved variants such as the improved symbiotic organisms search algorithm (ISOS) and modified symbiotic organisms search algorithm (MSOS).


2017 ◽  
Author(s):  
José. P.G. Carvalho ◽  
Afonso C.C. Lemonge ◽  
Érica C.R. Carvalho ◽  
Patrícia H. Hallak ◽  
Heder S. Bernardino

2017 ◽  
Vol 57 (2) ◽  
pp. 547-577 ◽  
Author(s):  
José P. G. Carvalho ◽  
Afonso C. C. Lemonge ◽  
Érica C. R. Carvalho ◽  
Patrícia H. Hallak ◽  
Heder S. Bernardino

Author(s):  
V. B. Venkayya ◽  
R. V. Grandhi

Abstract In this paper, design optimization of aircraft wing structures with multiple frequency constraints is considered. An optimality criterion algorithm along with a scaling procedure has been used. Large scale structural design problems were considered for demonstrating the reliability and efficiency of the algorithm. A simplified fighter wing, an intermediate complexity wing, and a large wing typical of a transport aircraft were considered as design examples. Design histories and the first few frequencies at the initial and final conditions are presented.


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