Vibration of Non-Uniform Beams

Garry M. Lindberg

Aeronautical Quarterly · 1963 · 38 citations · 1 references

Concepts

Abstract

Summary A method of deriving a dynamic stiffness matrix for any non-uniform beam is presented. In particular, the case of a linearly tapered cantilever beam is considered, and excellent results are found with the use of only a few elements.

References

1