Zobrazeno 1 - 7
of 7
pro vyhledávání: '"R. A. Tsarapkin"'
Publikováno v:
Combustion, Explosion, and Shock Waves. 57:74-82
An experimental method for determining the critical pressure perturbations leading to acoustic instability in combustion chambers of liquid-propellant rocket engines has been developed and used to estimate the stability of the working process. The me
Publikováno v:
Vestnik Mashinostroeniya. :15-21
An experimental method is proposed for estimating the damping decrements of pressure fluctuations in the combustion chambers of forced rocket engines. The method is based on the statistical processing of noise pressure pulsations in the vicinity of n
Autor:
V. I. Biryukov, R. A. Tsarapkin
Publikováno v:
Russian Engineering Research. 39:6-12
The damping decrements of pressure fluctuations in the combustion chambers of liquid-propellant rocket engines may be estimated on the basis of hard excitation of acoustic vibrations of a specific mode. A device for hard excitation of high-frequency
Autor:
Salgansky, E. A.1 (AUTHOR) sea@icp.ac.ru, Lutsenko, N. A.2,3 (AUTHOR), Yanovsky, L. S.1,4 (AUTHOR)
Publikováno v:
Combustion, Explosion, & Shock Waves. Jun2022, Vol. 58 Issue 3, p312-317. 6p.
Autor:
Astakhov, Sergei, Biryukov, Vasily
Publikováno v:
E3S Web of Conferences; 11/16/2023, Vol. 446, p1-8, 8p
Autor:
Biryukov, V. I.1 (AUTHOR) aviatex@mail.ru, Ivanov, V. N.2 (AUTHOR), Tsarapkin, R. A.1,2 (AUTHOR)
Publikováno v:
Combustion, Explosion, & Shock Waves. Jan2021, Vol. 57 Issue 1, p74-82. 9p.
Autor:
Biryukov, V. I., Tsarapkin, R. A.
Publikováno v:
Russian Engineering Research; Jan2019, Vol. 39 Issue 1, p6-12, 7p