Optimization of dynamic performance for a ground catapult with reusable supply of the working fluid


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Resumo

A task of minimizing the guide length of a ground catapult was set in order to ensure the mobility for unmanned aircraft systems. A scheme with reusable supply of the working fluid into the pneumatic drive cylinder was proposed. A method of parametric optimization of dynamic performance for a catapult was formulated. The method and models were verified with respect to the basic integral indicators.

Sobre autores

A. Ambrozhevich

N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”

Email: sereda_vlad@ukr.net
Ucrânia, ul. Chakalova 17, Kharkiv, 61070

K. Migalin

OOO HPF Rotor

Email: sereda_vlad@ukr.net
Rússia, ul. Rodiny 32, selo Podstepki, Stavropol’skii raion, Samara oblast, 445000

V. Sereda

N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”

Autor responsável pela correspondência
Email: sereda_vlad@ukr.net
Ucrânia, ul. Chakalova 17, Kharkiv, 61070

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Declaração de direitos autorais © Allerton Press, Inc., 2016