Method is set forth briefly verified by recalculation of investigation of gust effects and applied to problem in airplane dynamics, longitudinal motion of airplane when gun with powerful recoil is fired.
Operator solutions in airplane dynamics
J Aeronautical Science
Journal of Aeronautical Sciences ; 3 , n 7 ; p 252-255
1936
4 pages
Article (Journal)
English
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NTIS | 1964
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