It has been demonstrated that maneuvering loads due to motions about all three axes of airplane can be readily determined analytically for sequence of control movement varying linearly with time up to specified value and then held constant; it will be found that, in general, linear sequence is most adaptable to limitations such as set up in maneuvering horizontal tail load problem.
Airplane maneuvering loads
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 13 , n 6
1946
7 pages
Bibliography
Article (Journal)
English
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Engineering Index Backfile | 1961
|Horizontal Tail Loads in Maneuvering Flight
NTIS | 1950
|