电邮这篇文章 Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System
- 作者: Makhrov V.P.1, Sorokin V.A.1, Yur’ev A.I.1
-
隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 60, 编号 4 (2017)
- 页面: 495-499
- 栏目: Flight Vehicle Design
- URL: https://journals.rcsi.science/1068-7998/article/view/230262
- DOI: https://doi.org/10.3103/S1068799817040031
- ID: 230262
如何引用文章
开放存取
##reader.subscriptionAccessGranted##
订阅存取
详细
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.
作者简介
V. Makhrov
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: v_machrov@yandex.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
V. Sorokin
Moscow Aviation Institute (National Research University)
Email: v_machrov@yandex.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
A. Yur’ev
Moscow Aviation Institute (National Research University)
Email: v_machrov@yandex.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
补充文件
