Aerodynamic optimal design for a glider with the supersonic airfoil based on the hybrid MIGA-SA method

Author:

Wang F.P.,Xu Y.,Zhang G.Q.,Zhang K.

Funder

National Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference15 articles.

1. The research on multi-objective optimal algorithms for aerodynamic design;Wang;Acta Aerodyn. Sin.,2011

2. Genetic algorithm based optimal design for vibration control of composite shell structures using piezoelectric sensors and actuators;Roy;Int. J. Mech. Mater. Des.,2009

3. Development of a helicopter blade FE model using MIGA optimal;Hong;AIAA J.,2004

4. Missile aerodynamic geometry optimal using genetic algorithms;Anderson;J. Spacecr. Rockets,2000

5. UAV aerodynamic design involving genetic algorithm and artificial neural network for wing preliminary computation;Boutemedjet;Aerosp. Sci. Technol.,2019

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