Method presented which, it is believed, will permit cg range of airplane to be substantially increased, as well as reduce control forces in more satisfactory manner than is customary; method provides cockpit control by which pilot may regulate elevator hinge moment characteristics according to estimate of airplane cg. Before Inst Aeronautical Sciences.
New method of longitudinal control for aircraft by use of adjustable angle of attack balance
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 10 , n 5
1943
9 pages
Article (Journal)
English
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