To read the full version of this content please select one of the options below:

The Gust‐Load Problem: The Results of Acceleration Data Obtained on Large and Small Commercial Aeroplanes in America

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 1 August 1937

Abstract

THE highly complex character of the gust‐load problem and the lack of knowledge of gust structure have led to the general use of gust‐strength criteria for aeroplane wings that are based on the concept of a “sharp‐edged” gust in which the aerodynamic phenomena are assumed to obey the laws of steady flow.

Citation

Rhode, R.V. (1937), "The Gust‐Load Problem: The Results of Acceleration Data Obtained on Large and Small Commercial Aeroplanes in America", Aircraft Engineering and Aerospace Technology, Vol. 9 No. 8, pp. 212-217. https://doi.org/10.1108/eb030211

Publisher

:

MCB UP Ltd

Copyright © 1937, MCB UP Limited