Zobrazeno 1 - 10
of 13
pro vyhledávání: '"N. I. Tillyayeva"'
Autor:
A. N. Kraiko, N. I. Tillyayeva
Publikováno v:
Fluid Dynamics. 57:911-922
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::22d417af2e449144cf596c15aaf89c64
https://doi.org/10.1134/s0015462822070072
https://doi.org/10.1134/s0015462822070072
Publikováno v:
Computational Mathematics and Mathematical Physics. 62:624-640
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d14f518280154cfd19878ac20023e0b7
https://doi.org/10.1134/s0965542522040121
https://doi.org/10.1134/s0965542522040121
Publikováno v:
Computational Mathematics and Mathematical Physics. 60:697-710
The stability of one-dimensional steady flows of an ideal (inviscid and non-heat-conducting) gas in channels of variable cross section with combustion in a structurally stable detonation wave is studied. The detonation wave represents a discontinuity
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c838c356dbd1a4f82d39c394929b2c0f
https://doi.org/10.1134/s096554252004017x
https://doi.org/10.1134/s096554252004017x
Publikováno v:
Computational Mathematics and Mathematical Physics. 59:610-629
Features of plane-parallel and axisymmetric flows of an ideal (inviscid and non-heat-conducting) gas with a straight sonic line are studied. The flows under study occur in symmetric and asymmetric plane nozzles and axisymmetric nozzles with circular
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1b354cbc8e458134bf154f6cddf76bc
https://doi.org/10.1134/s0965542519040079
https://doi.org/10.1134/s0965542519040079
Publikováno v:
Journal of Applied Mathematics and Mechanics. 79:250-263
Axisymmetric conical flows (CF) without swirling and their unsteady cylindrically and spherically symmetric self-similar analogues with a self-similarity exponent of unity are considered in the approximation of an ideal (inviscid and non-heat-conduct
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c51ce35c561b58cffd68c651e817360e
https://doi.org/10.1016/j.jappmathmech.2015.09.005
https://doi.org/10.1016/j.jappmathmech.2015.09.005
Publikováno v:
Journal of Applied Mathematics and Mechanics. 76:451-465
The problem of the amplification of weak shock waves when a supersonic flow approaches the axis of symmetry and they are reflected from this axis is considered within the framework of an ideal (non-viscous and non-heat-conducting) gas model. A non-li
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce5799a6340008be66d790e1025a2a3c
https://doi.org/10.1016/j.jappmathmech.2012.09.013
https://doi.org/10.1016/j.jappmathmech.2012.09.013
Publikováno v:
Journal of Applied Mathematics and Mechanics. 67:703-730
The problem of constructing optimum or close to optimum nose-shapes of bodies of revolution of fixed aspect ratio in a supersonic flow is solved within the framework of a perfect (inviscid and non-heat-conducting) gas. Their contour includes the fron
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::498b7487158d6a3193ff4418f1d3789b
https://doi.org/10.1016/s0021-8928(03)90043-8
https://doi.org/10.1016/s0021-8928(03)90043-8
Publikováno v:
Fluid Dynamics. 38:482-490
Numerical simulation is used to study the gasdynamics of annular cumulative nozzles. The class of nozzles considered includes those with a flat-ended plug and plugs of different length. The thrust performance of cumulative nozzles is determined over
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fd9fc7a70d15dfe232015feef7f302a5
https://doi.org/10.1023/a:1025158425387
https://doi.org/10.1023/a:1025158425387
Publikováno v:
Fluid Dynamics. 37:637-648
The effect of transonic flow nonuniformity on the profiling of optimal plug nozzles is studied in the inviscid gas approximation. Sonic and supersonic regions providing maximum thrust for given nozzle dimensions and a given outer pressure are designe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cd973ffda5487b0a53c4daa485b7f345
https://doi.org/10.1023/a:1020653605889
https://doi.org/10.1023/a:1020653605889
Publikováno v:
Fluid Dynamics. 37:834-846
The flows in Laval nozzles with a ero-length region of abrupt constriction and in nozzles with smooth entrance regions are studied on the basis of the Reynolds equations supplemented by a differential turbulence model. It is established that the visc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1db07c824565cab0fdaa808e5547bdd5
https://doi.org/10.1023/a:1021392907861
https://doi.org/10.1023/a:1021392907861