The purpose of this report is to indicate what effect the distortion of a typical loaded wing truss will have upon the load distribution. The case of high angle of incidence may be dismissed immediately from consideration as the loads on the front and rear trusses are balanced, and consequently there will be little angular distortion. A given angular distortion will have the maximum effect upon load distribution in the region of the angle of no-lift, because the slope of the lift curve is highest here, and it is here that the greatest angular distortion will occur, because the load on the front truss acts downward while the load on the rear truss acts upward.
Torsion of wing trusses at diving speeds
1921-01-01
Sonstige
Keine Angabe
Englisch
Torsion of wing trusses at diving speeds
SLUB | 1920
|Torsion of wing trusses at diving speeds
Engineering Index Backfile | 1920
Torsion of wing trusses at diving speeds
TIBKAT | 1920
|