Effect of wall roughness on secondary flow choking in supersonic air ejector with adjustable motive nozzle
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24210%2F23%3A00011180" target="_blank" >RIV/46747885:24210/23:00011180 - isvavai.cz</a>
Výsledek na webu
<a href="https://www.sciencedirect.com/science/article/pii/S0142727X2300067X" target="_blank" >https://www.sciencedirect.com/science/article/pii/S0142727X2300067X</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1016/j.ijheatfluidflow.2023.109168" target="_blank" >10.1016/j.ijheatfluidflow.2023.109168</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Effect of wall roughness on secondary flow choking in supersonic air ejector with adjustable motive nozzle
Popis výsledku v původním jazyce
Wall roughness is present to a certain extent in all engineering devices and systems. However, it is rarely considered during numerical simulations of supersonic ejectors. In this study, the effect of wall roughness on choking within a supersonic ejector with an adjustable motive nozzle was investigated in detail. Wall roughness was studied through numerical simulations. Characteristic curves showed that roughness had almost no influence on secondary flow choking when choking occured geometrically before the mixing chamber. By contrast, when choking occurred within the mixing chamber, its phenomenology was significantly altered by wall roughness. In addition, the results confirmed the ability of an ejector to switch from the on-design working regime to the off-design one when wall roughness is considered. The numerical results were also compared with available experimental data. Accounting for wall roughness in the numerical analysis significantly improved the agreement between the experimental and numerical data, especially in terms of wall static pressure distributions. This study sheds light on secondary flow choking within a supersonic ejector considering wall roughness.
Název v anglickém jazyce
Effect of wall roughness on secondary flow choking in supersonic air ejector with adjustable motive nozzle
Popis výsledku anglicky
Wall roughness is present to a certain extent in all engineering devices and systems. However, it is rarely considered during numerical simulations of supersonic ejectors. In this study, the effect of wall roughness on choking within a supersonic ejector with an adjustable motive nozzle was investigated in detail. Wall roughness was studied through numerical simulations. Characteristic curves showed that roughness had almost no influence on secondary flow choking when choking occured geometrically before the mixing chamber. By contrast, when choking occurred within the mixing chamber, its phenomenology was significantly altered by wall roughness. In addition, the results confirmed the ability of an ejector to switch from the on-design working regime to the off-design one when wall roughness is considered. The numerical results were also compared with available experimental data. Accounting for wall roughness in the numerical analysis significantly improved the agreement between the experimental and numerical data, especially in terms of wall static pressure distributions. This study sheds light on secondary flow choking within a supersonic ejector considering wall roughness.
Klasifikace
Druh
J<sub>imp</sub> - Článek v periodiku v databázi Web of Science
CEP obor
—
OECD FORD obor
20303 - Thermodynamics
Návaznosti výsledku
Projekt
—
Návaznosti
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Ostatní
Rok uplatnění
2023
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název periodika
International Journal of Heat and Fluid Flow
ISSN
0142-727X
e-ISSN
—
Svazek periodika
103
Číslo periodika v rámci svazku
OCT
Stát vydavatele periodika
US - Spojené státy americké
Počet stran výsledku
15
Strana od-do
—
Kód UT WoS článku
001036810300001
EID výsledku v databázi Scopus
2-s2.0-85162228005