A series of calculations of the dynamic response of airplane wings to gusts were made with the purpose of showing the relative response of a reference airplane, the DC-3 airplane, and of newer types of airplanes represented by the DC-4, DC-6, and L-49 airplanes. Additional calculations were made for the DC-6 airplane to show the effects of speed and altitude. On the basis of the method of calculation used and the conditions selected for analysis, it is indicated that: 1) The newer airplanes show appreciably greater dynamic stress in gusts then does the reference airplane; 2) Increasing the forward speed or the operating altitude results in an increase of the dynamic stress ratio for the gust with a gradient distance of 10 chords.
Calculations of the Dynamic Stress of Several Airplane Wings in Various Gusts
1948-07-12
Sonstige
Keine Angabe
Englisch
Stresses Produced in Airplane Wings by Gusts
NTRS | 1932
|Investigation of dynamic response of airplane wings to gusts
Engineering Index Backfile | 1947
|Dynamic stress calculations for two airplanes in various gusts
Engineering Index Backfile | 1941
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