A study was conducted of the asymmetric load on the wing of a Canberra aircraft under turbulent conditions. The asymmetric part is separated from the symmetric part as far as is possible with the available data. The relationship of the asymmetric part to the rolling acceleration is analyzed. (Author)
Asymmetric Wing Loads on a Canberra Aircraft During Flight in Turbulence
1974
28 pages
Report
Keine Angabe
Englisch
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