TY - JOUR AB - THE mathematically exact determination of the stress distribution in a two‐spar skin‐covered wing is, in the present state of knowledge, an impossibility, and is in fact quite unnecessary, since only a reasonable approximation is required. The theory outlined in this article will, it is hoped, give a reasonable approximation for a reasonable amount of work, while taking into account as many variables as possible. VL - 13 IS - 6 SN - 0002-2667 DO - 10.1108/eb030780 UR - https://doi.org/10.1108/eb030780 AU - Goodey W.J. PY - 1941 Y1 - 1941/01/01 TI - Two‐Spar Wing Stress Analysis: A Theory Giving a Reasonable Approximation to the Stress‐Distribution in a Skin‐Covered Plane T2 - Aircraft Engineering and Aerospace Technology PB - MCB UP Ltd SP - 150 EP - 153 Y2 - 2024/03/28 ER -