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Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System
Authors:V. P. Makhrov  V. A. Sorokin  A. I. Yur’ev
Affiliation:1.Moscow Aviation Institute (National Research University),Moscow,Russia
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.
Keywords:
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