Zobrazeno 1 - 10
of 1 511
pro vyhledávání: '"total air temperature"'
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 15, Iss 5, Pp 1437-1449 (2022)
Experiments on a two-phase rotating detonation combustor operating with gasoline and high total temperature air were conducted to investigate the initiation characteristics, operation mode, and propagation characteristics of a two-phase rotating deto
Externí odkaz:
https://doaj.org/article/20257b480cbf46569c4ba98b294bb07d
Autor:
Ihor Ivanyuk, Yaroslav Fuchylo
Publikováno v:
Наукові праці Лісівничої академії наук України, Vol 20, Pp 57-63 (2020)
The important economic, ecological and social functions of the forests with the participation of English oak are presented., The study of their growth conditions, development and biological stability in different natural zones under the climatic fact
Externí odkaz:
https://doaj.org/article/365c54fb7d514afab3128ce6fafc6ef0
Publikováno v:
Chinese Journal of Aeronautics. 35:192-208
In this paper, the combustion characteristics of kerosene-fueled supersonic combustor under the conditions of Mach number 2.0, the total temperature at 700 K and the total pressure at 520 kPa (simulated flight Mach number at 3.5) were studied by usin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::21955b46b4d7584ee5f25ca6288b98ab
https://doi.org/10.1016/j.cja.2021.10.029
https://doi.org/10.1016/j.cja.2021.10.029
Publikováno v:
Chinese Journal of Aeronautics. 35:202-219
Front Variable Area Bypass Injector (Front-VABI) is a component of the Adaptive Cycle Engine (ACE) with important variable-cycle features. The performance of Front-VABI has a direct impact on the performance and stability of ACE, but the current ACE
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e083ebb90b83236948912c00b8e259be
https://doi.org/10.1016/j.cja.2021.08.034
https://doi.org/10.1016/j.cja.2021.08.034
Publikováno v:
Acta Astronautica. 189:722-732
An especial air-breathing continuous rotating detonation engine without a centerbody is proposed to reduce energy loss and simplify the structure, which is analogous to a typical scramjet combustor with the cavity. Non-premixed ethylene/air rotating
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1d810dcc4b96fecef20595786d1a9a03
https://doi.org/10.1016/j.actaastro.2021.09.009
https://doi.org/10.1016/j.actaastro.2021.09.009
Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator
Publikováno v:
Acta Astronautica. 188:416-425
SparkJet (SPJ) actuator was used to control shock and shock-on-shock interaction in high-enthalpy hypersonic flow with a total temperature of 4490 K and Mach number 6.9 for the first time. Aiming at the characteristics of rarefied gas in hypersonic f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29200312e7c3b01c4e398e2a1bfa5beb
https://doi.org/10.1016/j.actaastro.2021.07.032
https://doi.org/10.1016/j.actaastro.2021.07.032
Publikováno v:
Acta Astronautica. 185:117-123
To estimate the vitiation effects of test air on flameholding and mode transition in a direct-connected dual mode combustor, an experimental study was conducted with two types of air heater (electric heater and methane combustion heater) at various k
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::355affd763373d9da26ea0984da9b43c
https://doi.org/10.1016/j.actaastro.2021.04.015
https://doi.org/10.1016/j.actaastro.2021.04.015
Publikováno v:
Journal of Thermal Science. 30:1421-1434
This paper presents a satisfactory numerical strategy to reliably evaluate the three-dimensional large-scale flow feature of multistage axial compressors in response to complex swirl distortion with acceptable computational cost. Under the theoretica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e306fcb60efc6a7cf8b29e5a25d8cfcc
https://doi.org/10.1007/s11630-021-1483-7
https://doi.org/10.1007/s11630-021-1483-7
Publikováno v:
Thermal Engineering. 68:337-346
Some rows of steam and gas turbines, with the exception of the first vanes, operate at the inlet flow conditions created by the upstream turbine stages. In particular, the conditions of the flow at the inlet of a low-pressure turbine vanes (LPT vanes
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::08f79581c2133c8144a116fc24c5b037
https://doi.org/10.1134/s0040601521050013
https://doi.org/10.1134/s0040601521050013
Publikováno v:
Acta Astronautica. 182:219-229
Effects of a jet emanating from the nose of a generic rocket in the opposite direction of the incoming freestream have been studied to determine the effects of the jet in reducing the drag and the heat loads on the rocket. The effects are comparative
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ee75f6634b951a7d8e82b27819865bd1
https://doi.org/10.1016/j.actaastro.2021.01.060
https://doi.org/10.1016/j.actaastro.2021.01.060