DESIGN AND CALCULATION OF AN AIRPLANE WING WITH TAKE-OFF WEIGHT TO 2000kg

Abstract

The task of this work was to design an aircraft wing for a maximum takeof weight of 2000kg. Basic characteristcs were chose according to the konwledge gained in this issue. The basic formula has been calculated baseload wing. In the design of the elementary program was used to Enginieer. Where were analyzed voltage. Under stress, the proposed design modifcations carried out.