Версия для печати

Vol. 3, no. 2, 2019

OMSK SCIENTIFIC BULLETIN. SERIES «AVIATION-ROCKET AND POWER ENGINEERING»

CONTENTS

MECHANICS

Yu. A. Burian, M. V. Silkov
Vibration isolation with quasi-zero stiffness effect

V. S. Korneyev, V. V. Shalay
Linearized mathematical model of rubber-cord shell

POWER AND CHEMICAL ENGINEERING

Yu. B. Galerkin, A. A. Drozdov
New version of Universal modeling method for centrifugal compressors calculation development

V. I. Karagusov, I. N. Pogulyaev
Average daily cooling capacity of radiation conditioning system

A. A. Malyshev, A. V. Zaitsev, K. F. Kuadio, K. V. Kisser
Experimental research of hydrodynamic characteristics during boiling of refrigerants
in minichannels using true parameters of phases

N. A. Raykovskiy, V. L. Yusha, A. V. Tretyakov, V. A. Zakharov, K. I. Kuznetsov
The method for studying temperature deformations of self-lubricating bearing friction units
of high-temperature low-flow turbine

V. V. Karabanova, A. D. Vanyashov, V. L. Yusha
Some features of implementation of design model of high-pressure centrifugal compressor stage with inlet guide vanes

T. V. Ryabova, A. B. Sulin, A. K. Rubtsov, S. S. Muraveinikov
Modeling of radiant heat exchange processes

A. Yu. Uss, A. V. Chernyshev, N. V. Atamasov
Development of calculation method and creation of vortex jet device to control gas flow

V. E. Scherba, A. V. Grigor’ev, A. V. Zanin
Mathematical model of working processes of piston hybrid power machine of volumetric action
with reduced fluctuations of gas pressure in discharge line

AVIATION AND ROCKET-SPACE ENGINEERING

V. N. Blinov, A. I. Lukyanchik, V. V. Shalay
The method of investigation of basic project parameters of microsatellite by random search

V. I. Trushlyakov, V. A. Urbansky
Study of unusable liquid propellant residues evaporation processes parameters in the tanks
of launch vehicle worked-off stage in microgravity

B. T. Suimenbayev, V. I. Trushlyakov, G. T. Yermoldina, Zh. B. Suimenbayeva, A. M. Bapyshev
The concept of reducing the man-made impact of launches of the promising Irtysh launch vehicle
in the impact areas of the Baikonur cosmodrome

V. S. Korneyev, S. A. Korneyev
Calculation-experimental method for determining the initial geometric parameters of rubber-cord shell of rotation

V. I. Karagusov
Anaerobic external combustion thermal engines

V. I. Gorbunkov, V. V. Shalay
Optic evaluation of erosion arcjet tungsten electrodes

V. I. Kuznetsov, A. Yu. Shander
Hartmann–Sprenger effect and its application on aircraft

E. V. Shendaleva, Kh. I. Khalimov
Design of experiments at bench tests of fuel supplying apparatus