Отправить статью по E-mail Optimization of dynamic performance for a ground catapult with reusable supply of the working fluid
- Авторы: Ambrozhevich A.1, Migalin K.2, Sereda V.1
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Учреждения:
- N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
- OOO HPF Rotor
- Выпуск: Том 59, № 4 (2016)
- Страницы: 441-446
- Раздел: 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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Аннотация
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.
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Об авторах
A. Ambrozhevich
N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Email: sereda_vlad@ukr.net
Украина, ul. Chakalova 17, Kharkiv, 61070
K. Migalin
OOO HPF Rotor
Email: sereda_vlad@ukr.net
Россия, ul. Rodiny 32, selo Podstepki, Stavropol’skii raion, Samara oblast, 445000
V. Sereda
N.E. Zhukovskii National Aerospace University “Kharkiv Aviation Institute”
Автор, ответственный за переписку.
Email: sereda_vlad@ukr.net
Украина, ul. Chakalova 17, Kharkiv, 61070
