Sineglazov, ViktorZiganshin, Anvar2017-03-172017-03-172015-10978-1-4673-6566-6http://er.nau.edu.ua/handle/NAU/25367Ukraine Section SP/AES Joint ChapterThe range of geometric parameters describing the airfoil form was determined. The computer aided design method to optimize these geometric parameters on the base of genetic algorithm was created.enаerodynamicsComputer Aided Design of Wing with Given CharacteristicsArticle