International Journal of Science, Engineering and TechnologyAuthors: Van Huy Khuat, Le Thanh Nguyen, Van Viet Vo
Abstract: This paper presents the results of a survey on the change in the lift coefficient of the wing profile when using flaps on the Ansys Fluent application platform. The use of these flaps is extremely important. They not only ensure safe and efficient takeoff and landing but also enable rapid takeoff to approach and destroy targets even under runway damage. The paper investigates the change in the lift coefficient of the wing with flaps using Ansys Fluent software. Using this method, it is possible to determine the parameters corresponding to each type of flap, calculate the lift coefficient in each case, and identify the causes of these parameter changes.
