Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System

被引：0

作者：

Makhrov V.P. ^{[1
]}

Sorokin V.A. ^{[1
]}

Yur’ev A.I. ^{[1
]}

机构：

[1] Moscow Aviation Institute (National Research University), Volokolamskoe shosse 4, Moscow

来源：

Russian Aeronautics | 2017年 / 60卷 / 4期

关键词：

annular wing; cavitation flow; gas flowrate;

D O I：

10.3103/S1068799817040031

中图分类号：

学科分类号：

摘要：

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. © 2017, Allerton Press, Inc.

引用

页码：495 / 499

页数：4

共 8 条

[1]

Tarasov E.V., Uvarov G.V., Vysokoskorostnaya podvodnaya raketa (High-Speed Underwater Rocket), (2013)

[2]

Degtyr' V.G., Pegov V.I., Gidrodinamika podvodnogo starta raket (Hydrodynamics of Underwater Rocket’s Start), (2009)

[3]

Barsukov V.D., Goldaev S.V., Studies of Open-Cycle Gas Generator Operation Stability in Aqueous Medium, Izv. Vuz. Av. Tekhnika, 48, 2, pp. 30-33, (2001)

[4]

Shishkov A.A., Rumyantsev B.V., Gazogeneratory raketnykh system (Gas Generators of the Rocket Systems), (1981)

[5]

Makhrov V.P., Hydrodynamics of Controlled Flows with Free Boundaries Formed by a Ring Type Wing used as an External Hydrodynamic Singularity, Vestnik MAI, 16, 5, pp. 264-273, (2009)

[6]

Makhrov V.P., Gidrodinamika kavitatsionnykh techenii formiruemykh vneshnimi gidrodinamicheskimi osobennostyami (Hydrodynamics of Cavity Flows Formed by External Hydrodynamic Singularities), (2011)

[7]

Rozhdestvenskii V.V., Kavitatsiya (Cavitation), (1977)

[8]

Belotserkovskii S.M., Tonkaya nesushchaya poverkhnost’ v dozvukovom potoke gaza (Thin Carrier Surface in Subsonic Flow of Gas), (1969)

← 1 →