Four different methods for determination of sideslip angle, vertical tail angle of attack, and vertical tail load during rolling pullout maneuver; airplane configurations considered are straight wing, swept wing, and delta wing type.
Analysis of rolling pull-out maneuver
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 23 , n 6 ; p 517-529
1956
13 pages
Article (Journal)
English
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