Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons Page: 13 of 29
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(a) Mode of operation when control force does not exceed sprny pre/oad.
(b) Mode of operation when spri/n /s compressed to defl/ct ab.
ty 3 -Jchem atic darczam sowiny prin c/e of operabon ofspriny A /lkaye.
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Imlay, Frederick H. & Bird, J. D. Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons, report, January 1944; (digital.library.unt.edu/ark:/67531/metadc61613/m1/13/: accessed February 20, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.