Publication Date:
2019-07-27
Description:
Free vibration of discretely stiffened cylindrical shells with arbitrary end conditions programmed for digital computer, considering flexure, extension, torsion and nonsymmetric stiffener cross section
Keywords:
STRUCTURAL MECHANICS
Type:
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, STRUCTURAL DYNAMICS AND AEROELASTICITY SPECIALIST CONFERENCE; APRIL 16, 17, 1969; NEW ORLEANS, LA.
Format:
text
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