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.
The Gust-Load Problem
The Results of Acceleration Data Obtained on Large and Small Commercial Aeroplanes in America
Aircraft Engineering and Aerospace Technology ; 9 , 8 ; 212-217
1937-08-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Emerald Group Publishing | 1941
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