Theoretical study demonstrating that control force of ordinary ailerons may be reduced to zero over range of deflections and at given flight condition by use of appropriate differential movement; approximates to ideal motion obtainable with simple linkage; chart for selection of appropriate crank arrangement; practical application of system.
Reduction of aileron operating force by differential linkage
Nat Advisory Committee Aeronautics -- Tech Notes
1936
13 pages
10 Supp sheets, Bibliography
Report
Englisch
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