Zobrazeno 1 - 10
of 79
pro vyhledávání: '"A. N. Shiplyuk"'
Publikováno v:
Thermophysics and Aeromechanics. 29:151-165
Autor:
S. O. Morozov, A. N. Shiplyuk
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Autor:
S. O. Morozov, A. N. Shiplyuk
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Publikováno v:
ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS.
Autor:
Denis G. Nalivaychenko, S. V. Lukashevich, Dmitrii A. Vnuchkov, Alexander N. Shiplyuk, Alexey Yu Melnikov, V. I. Zvegintsev, Tatiana A. Kiseleva, S. M. Frolov, Valentin Alexeevich Kislovsky
Publikováno v:
Journal of Propulsion and Power. 37:20-28
The gasification process of a low-melting fuel (polypropylene) in a high-temperature flow of inert gas (nitrogen) has been studied experimentally, implying the application to solid-fuel ramjets. Th...
Autor:
A. N. Shiplyuk, S. O. Morozov
Publikováno v:
Thermophysics and Aeromechanics. 27:633-642
The influence of a local change in surface temperature of a contoured nozzle corresponding to the Mach number M = 6 on the boundary layer stability and laminar-turbulent transition is numerically studied. The profiles of the laminar boundary layer ar
Autor:
D. A. Vnuchkov, S. V. Lukashevich, Valentin Alexeevich Kislovsky, S. M. Frolov, Alexander N. Shiplyuk, T.A. Kiseleva, D. G. Nalivaychenko, A. Yu. Melnikov, V. I. Zvegintsev
Publikováno v:
International Journal of Hydrogen Energy. 45:9098-9112
The airflow heated by combustion of hydrogen–oxygen mixture to a temperature ranging from 300 to 1500 K is used for the gasification of a low-melting hydrocarbon material – polypropylene (PP) in a flow-type reactor. The yield of PP gasification p
Publikováno v:
IUTAM Laminar-Turbulent Transition ISBN: 9783030679019
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7afc58323db4f7028f20440c3930cefb
https://doi.org/10.1007/978-3-030-67902-6_53
https://doi.org/10.1007/978-3-030-67902-6_53
Publikováno v:
Experiments in Fluids. 62
The effect of surfaces with streamwise microgrooves on the development of natural disturbances in a hypersonic boundary layer is experimentally studied. The experiments are performed on a sharp cone at the free-stream Mach number M∞ = 5.8. Microgro
Publikováno v:
Thermophysics and Aeromechanics. 25:793-800
The present work was devoted to an experimental study of small angles of attack and cone nose bluntness on the efficiency of stabilization of high-frequency disturbances in hypersonic boundary layer with a passive porous coating. The experiments were