Distribution of Load over Wing Tips and Stress Analysis
It is a well known fact, that load per inch run of a wing drops off in proximity of wing tip. The necessity of taking this drop into account in strength computations was recognized long ago, and several approximate methods were in use. Study of pressure distribution along model wings was made by the National Physical Laboratory, and led to the conclusion, that distribution of the load over a wing tip is practically independent of the plan form of the tip.
By B. V. Korvin-Kroukovsky