Methods for quantitative prediction of behavior following initial misalignment on catapult in terms of time histories of motion; both single pendant towing arrangement and case of V-bridle considered; comparison shown between calculations and dynamically similar model typifying current jet fighter parameters.
Prediction of yawing stability characteristics of airplanes during catapulting
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 8
1952
11 pages
Aufsatz (Zeitschrift)
Englisch
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