Analysis is made by means of equations of motions with aircraft pitch and fundamental wing bending degrees of freedom; possibility of employing technique of large concentrated masses at wing tips in nuclear or military aircraft.
Effects of large wing-tip masses on oscillatory stability of wing bending coupled with airplane pitch
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 12-29-58A
1959
32 pages
Report
English
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