Email this article Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System
- Authors: Makhrov V.P.1, Sorokin V.A.1, Yur’ev A.I.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 60, No 4 (2017)
- Pages: 495-499
- Section: 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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Abstract
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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About the authors
V. P. Makhrov
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: v_machrov@yandex.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
V. A. Sorokin
Moscow Aviation Institute (National Research University)
Email: v_machrov@yandex.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
A. I. Yur’ev
Moscow Aviation Institute (National Research University)
Email: v_machrov@yandex.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
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