电邮这篇文章 Optimization of dynamic performance for a ground catapult with reusable supply of the working fluid
- 作者: Ambrozhevich A.V.1, Migalin K.V.2, Sereda V.A.1
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隶属关系:
- N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
- OOO HPF Rotor
- 期: 卷 59, 编号 4 (2016)
- 页面: 441-446
- 栏目: 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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详细
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.
作者简介
A. Ambrozhevich
N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Email: sereda_vlad@ukr.net
乌克兰, ul. Chakalova 17, Kharkiv, 61070
K. Migalin
OOO HPF Rotor
Email: sereda_vlad@ukr.net
俄罗斯联邦, ul. Rodiny 32, selo Podstepki, Stavropol’skii raion, Samara oblast, 445000
V. Sereda
N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
编辑信件的主要联系方式.
Email: sereda_vlad@ukr.net
乌克兰, ul. Chakalova 17, Kharkiv, 61070
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