Control of Nozzle Flow Using Rectangular Ribs at Sonic and Supersonic Mach Numbers

被引:0
|
作者
Sethuraman, Vigneshvaran [1 ]
Rajendran, Parvathy [1 ]
Khan, Sher Afghan [2 ]
Aabid, Abdul [3 ]
Baig, Muneer [3 ]
机构
[1] Univ Sains Malaysia, Sch Aerosp Engn, Engn Campus, Nibong Tebal 14300, Pulau Pinang, Malaysia
[2] Int Islamic Univ Malaysia, Fac Engn, Dept Mech & Aerosp Engn, Kuala Lumpur 53100, Malaysia
[3] Prince Sultan Univ, Coll Engn, Dept Engn Management, POB 66833, Riyadh 11586, Saudi Arabia
来源
关键词
Base pressure; internal flows; ribs; suddenly expanded flow; wall pressure; CAVITIES;
D O I
10.32604/fdmp.2024.049441
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This study deals with base pressure management in a duct for various values of the Mach number (M), namely, Mach number corresponding to sonic and four supersonic conditions. In addition to the Mach number, the nozzle pressure ratio (NPR), the area ratio, the rib dimension, and the duct length are influential parameters. The following specific values are examined at M = 1, 1.36, 1.64, and 2, and NPRs between 1.5 and 10. The base pressure is determined by positioning ribs of varying heights at predetermined intervals throughout the length of the square duct. When the level of expansion is varied, it is seen that the base pressure initially drops for overexpanded flows and increases for under-expanded flows. When ribs are present, the flow field in the duct and pressure inside the duct fluctuate as the base pressure rises. Under-expanded flows can achieve a base pressure value that is suitably high without experiencing excessive changes in the duct flow in terms of static pressure if a rib height around 10% of the duct height close to the nozzle exit is considered. Rectangular rib passive control does not negatively affect the duct's flow field.
引用
收藏
页码:1847 / 1866
页数:20
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