Email this article Optimization of dynamic performance for a ground catapult with reusable supply of the working fluid
- Authors: Ambrozhevich A.V.1, Migalin K.V.2, Sereda V.A.1
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Affiliations:
- N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
- OOO HPF Rotor
- Issue: Vol 59, No 4 (2016)
- Pages: 441-446
- Section: Aircraft Equipment
- URL: https://journals.rcsi.science/1068-7998/article/view/229830
- DOI: https://doi.org/10.3103/S1068799816040012
- ID: 229830
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Abstract
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.
About the authors
A. V. Ambrozhevich
N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Email: sereda_vlad@ukr.net
Ukraine, ul. Chakalova 17, Kharkiv, 61070
K. V. Migalin
OOO HPF Rotor
Email: sereda_vlad@ukr.net
Russian Federation, ul. Rodiny 32, selo Podstepki, Stavropol’skii raion, Samara oblast, 445000
V. A. Sereda
N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Author for correspondence.
Email: sereda_vlad@ukr.net
Ukraine, ul. Chakalova 17, Kharkiv, 61070
