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
1936
4 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
NTIS | 1964
|Airplane spoiler manufacturing method, airplane spoiler and airplane
European Patent Office | 2015
|Dynamics of airplanes and airplane structures
Engineering Index Backfile | 1931