Enviar artigo por via de e-mail Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System
- Autores: Makhrov V.P.1, Sorokin V.A.1, Yur’ev A.I.1
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Afiliações:
- Moscow Aviation Institute (National Research University)
- Edição: Volume 60, Nº 4 (2017)
- Páginas: 495-499
- Seção: Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230262
- DOI: https://doi.org/10.3103/S1068799817040031
- ID: 230262
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Resumo
We determine the behavior of onboard gas-generator flowrate for generating the cavitation flow around a hybrid aerial underwater vehicle by using an annular wing on the underwater trajectory section.
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Sobre autores
V. Makhrov
Moscow Aviation Institute (National Research University)
Autor responsável pela correspondência
Email: v_machrov@yandex.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
V. Sorokin
Moscow Aviation Institute (National Research University)
Email: v_machrov@yandex.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
A. Yur’ev
Moscow Aviation Institute (National Research University)
Email: v_machrov@yandex.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
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