TY  - JOUR
AB  - IN Part I of this paper, the basic equations were established for the various modes of instability of flat sandwich panels subjected to lengthwise compression. Whilst these equations are valuable in determining the strength of a given panel they do not give a direct indication of the cross‐sectional dimensions of a panel required to carry a given load, especially if the panel is to be the optimum, i.e. of minimum weight.
VL  - 32
IS  - 8
SN  - 0002-2667
DO  - 10.1108/eb033287
UR  - https://doi.org/10.1108/eb033287
AU  - Heath W.G.
PY  - 1960
Y1  - 1960/01/01
TI  - Sandwich Construction: Correlation and Extension of Existing Theory of Flat Panels Subjected to Lengthwise Compression
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 230
EP  - 235
Y2  - 2024/04/18
ER  -