Two methods of obtaining balancing effect are explained, (1) by moving pivot points aft to center of pressure about 20 per cent aft leading edge on rectangular surface, and (2) by moving center of pressure forward to pivot or hinge line by extension of part of surface in front of hinge line.
Balanced control surfaces on aircraft
Aviation
Aviation ; 8 , n 2 ; p 57-58
1920
2 pages
4 Figs.
Aufsatz (Zeitschrift)
Englisch
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