Finite element analysis (FEA) modeling on adhesive joint for composite fuselage model
F. Mustapha1, N. W. Sim1 and A. Shahrjerdi2*
1Department of Aerospace Engineering, Universiti Putra Malaysia, 43400 UPM Serdang, Selangor, Malaysia.
2Department of Mechanical Engineering, Malayer University, Iran.
Email: [email protected]