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	Elastic stresses and deflections under uniform pressure of flat rectangular sandwich panels; all edges simply-supported (isotropic face plates and orthotropic cores of zero flexural stiffness).
DATA Item	76013
KEYWORD	deflection, flat, honeycomb, panel, pressure, rectangular, sandwich, stress
ISBN	0 85679 149 0
ABSTRACT	ESDU 76013 gives graphs enabling the maximum deflection and the maximum direct and shear stresses to be found in initially flat simply-supported panels. The method assumes the face plates have the same Poissonchr(39)s ratio but they can have different thicknesses and moduli of elasticity. The curves were calculated from elastic small deflection theory assuming the face plates to be thin and the core infinitely stiff in the through-thickness direction. These assumptions will be valid for panel thickness/face plate thickness greater than 6, for panel length/panel thickness greater than 10, and for deflection/panel thickness less than 0.5.