Laboratory Homepage

HOME LOGIN JOIN ID/PASSWORD FIND KOREAN

Undergraduate Courses Lecture

Mechanics of Aerospace Structures

  • Overview of the subject

    In this class, methodologies to compute an overall load path and approximate stress distribution will be learned by idealizing a realistic aircraft structures, in order to adopt them in the preliminary and detail design. Since the practical computations are conducted by numerical analysis, physical and mechanical aspects will rather be emphasized by going through simple analysis problems involving low-order numerical computation.

  • T.A

    N/A

  • Grade

    Attendance (0%) / Test (Mid 0%, Final 0%) / Homework (0%)

  • References

    Bauchau, O. A. and Craig, J. I., “Structural Analysis with Application to Aerospace Structures,” Springer, 2009.
    Curtis, H. D., “Fundamentals of Aircraft Structural Analysis,” IRWIN, 1997.
    Arnold, E., “Aircraft Structures for Engineering students,” T.H.G. Megson, 1990.