국내 최대 기계 및 로봇 연구정보

공학설계D/B

공학설계D/B 게시판 내용
Volume Title	Structures
Volume No	Cylinders and pipes - buckling under compression, bending, torsion with internal pressure, collapse under external pressure, flat/torispherical head stresses, bend flexibility. Sandwich panels under normal loading - deflections\stresses under pressure, core stresses due to local load.
DATA Title	Stresses in the core of a sandwich panel under local normal loading.
DATA Item	73025
KEYWORD	core, honeycomb, loading, local, normal, panel, sandwich, stress
ISBN	0 85679 049 4
ABSTRACT	Data are given for stresses under local loading applied remote from the panel edges. The panels have identical isotropic face plates and a core with equal shear stiffness in all planes through the depth. The loading is assumed to be axisymmetrically distributed over a circular area but the shape of the distribution can be varied. Graphs give the maximum shear and compressive stresses in the core as a function of core and faceplate properties and dimensions. Guidance is given on a choice of load distribution.