Zobrazeno 1 - 8
of 8
pro vyhledávání: '"G. A. Kolton"'
Publikováno v:
Vestnik Samarskogo Gosudarstvennogo Tehničeskogo Universiteta. Seriâ: Fiziko-Matematičeskie Nauki, Vol 1(18), Pp 18-25 (2009)
Abstract: The plane auto model problem of the in viscid gas motion beyond intensive shock wave is studied. It is supposed, that shock wave front approaches some curve, the form of which is known. Solution is constructed in the form of series on the s
Externí odkaz:
https://doaj.org/article/13de147648cf44f99298652ce31c55fb
Publikováno v:
2015 International Conference on Mechanics - Seventh Polyakhov's Reading.
The spatial hypersonic problem of the flow past a thin wing is studied. The head shock wave is attached to the wing leading edge, at least, at one point. The thin shock layer method and the Euler-Amper transformation are applied to the problem under
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::59c64bbeeac1a40c8750dd9bf89d630a
https://doi.org/10.1109/polyakhov.2015.7106717
https://doi.org/10.1109/polyakhov.2015.7106717
Autor:
G. A. Kolton, V. I. Bogatko
Publikováno v:
Fluid Dynamics. 32:92-102
The transient regime in gas flow past a stepwise accelerated body is analyzed by the method of singular perturbations at small Froude numbers. A marked effect of the initial conditions on the shock layer gas flow is demonstrated. The problem of flow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::90196ac65420ab35640f2371a6d6745b
https://doi.org/10.1007/bf02697942
https://doi.org/10.1007/bf02697942
Autor:
V. I. Bogatko, G. A. Kolton
Publikováno v:
Fluid Dynamics. 18:243-247
Experimental investigations [1] show that when allowance is made for the real properties of a gas it is possible to have a regime of regular reflection of a shock wave from the surface of a wedge in which the reflected shock wave is attached to the t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::41243aaa0c6b46fe3280cf59f81ae9c9
https://doi.org/10.1007/bf01091112
https://doi.org/10.1007/bf01091112
Autor:
V. I. Bogatko, G. A. Kolton
Publikováno v:
Fluid Dynamics. 9:722-727
The problem of irregular reflection of a strong shock wave from a rigid wall has been studied [1–3] mainly within the framework of the linear theory. It has been found that near the front of a shock wave there exist a region of large gradients of g
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::87db53e36b9a18747def1563692f6983
https://doi.org/10.1007/bf01017417
https://doi.org/10.1007/bf01017417
Publikováno v:
Fluid Dynamics. 14:548-554
In a formulation analogous to [1–3], a study is made of the flow of a uniform homogeneous hypersonic ideal gas over the windward side of a slender wing whose surface profile depends on the time. The problem is solved by the thin shock layer method
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e2c8fa49cb711e003231d69139fd0fc2
https://doi.org/10.1007/bf01051255
https://doi.org/10.1007/bf01051255
Autor:
V. I. Bogatko, G. A. Kolton
Publikováno v:
Fluid Dynamics. 11:919-924
The axisymmetrical problem concerning Mach reflection of an intense shock wave from the surface of a thin cone is considered in a formulation similar to that of [1].
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b1a4a5766fa0fe3bdb1a9cbe4d9c99e1
https://doi.org/10.1007/bf01026415
https://doi.org/10.1007/bf01026415
Autor:
V. V. Stal’skii, G. A. Kolton
Publikováno v:
Soviet Mining Science. 14:616-622
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ad8f416c0d2b8bc64815b25477b6ea3f
https://doi.org/10.1007/bf02499499
https://doi.org/10.1007/bf02499499