中国机械工程学会生产工程分会知识服务平台

期刊


ISSN1068-7998
刊名Russian Aeronautics
参考译名俄罗斯航空学
收藏年代2003~2023



全部

2003 2004 2005 2006 2009 2010
2011 2012 2013 2014 2015 2016
2017 2018 2019 2020 2021 2022
2023

2017, vol.60, no.1 2017, vol.60, no.2 2017, vol.60, no.3 2017, vol.60, no.4

题名作者出版年年卷期
Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming SystemV. P. Makhrov; V. A. Sorokin; A. I. Yur’ev20172017, vol.60, no.4
Numerical Simulation of the Flow in the Scramjet Combustion Chamber Taking into Account Nonequilibrium Chemical ReactionsA. M. Molchanov; A. S. Myakochin20172017, vol.60, no.4
Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure BendingV. K. Belov; L. P. Zheleznov; T. S. Ognyanova20172017, vol.60, no.4
Lowering the Systematic Error in Measurements of Local Heat Transfer Coefficient by Electric Heating of a Plane WallN. S. Dushin; N. I. Mikheev; I. M. Gazizov; I. A. Davletshin20172017, vol.60, no.4
A Technique of Object Detection Using Information about Changes in the Terrain ImageD. I. Miftakhutdinov; I. S. Rizaev; M. P. Shleimovich20172017, vol.60, no.4
Influence of Simplifying a Geometrical Model of the Gas Turbine Engine Combustion Chamber on the Results of Numerical ModelingYu. B. Aleksandrov; V. B. Yavkin; A. N. Sabirzyanov20172017, vol.60, no.4
Dynamic Stability of a Cylindrical Shell under Alternating Axial External PressureV. N. Bakulin; E. N. Volkov; A. I. Simonov20172017, vol.60, no.4
On a Problem of Optimal Control of the Laminar Boundary Layer in Supersonic Flows on Constant-Pressure SurfacesT. K. Garaev; D. M. Osadchaya20172017, vol.60, no.4
Algorithms of Constructing the Regions of Initial States for Unmanned Winged GlidersV. T. Grumondz; E. I. Karpezhnikov; M. A. Polishchuk; M. V. Polishchuk20172017, vol.60, no.4
On Relationship of Flow Swirl Parameters and Gas-Dynamic Efficiency of Gas Turbine Engine Interturbine Transition DuctA. E. Remizov; V. V. Vyatkov; V. V. Lebedev20172017, vol.60, no.4
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