Fusalage and Tail of Competition Model Airplane

This bachelor’s thesis deals with empennage and fuselage design of new aircraft for design competition SAE Aero Design East 2020. The introduction is focused on regulations of this competiton and their subsequent analysis. The research part of the thesis takes in consideration possible configurations of the empennage and fuselage and their basic parameters. The most suitable configurations are compared and basic stability and load calculations are done. In the last part structural design is completed