An analysis of symmetric reinforcement of graphite/epoxy honeycomb sandwich panels with a circular cutout under uniaxial compressive loading
Published: 1985
Language: eng
Number of pages: 342
Subjects: Aeronautics
Notes: Available from National Technical Information Service, Springfield, Va.

Thesis (M.S. in A.E.) Naval Postgraduate School, 1985.

Bibliography:  p. 340-341.

c.1 - 215609, c.2 - 215610