دورية أكاديمية

Influence of Incident Shock on Fuel Mixing in Scramjet

التفاصيل البيبلوغرافية
العنوان: Influence of Incident Shock on Fuel Mixing in Scramjet
المؤلفون: Chao Wang, Hongbo Wang, Yixin Yang, Xu Liu
المصدر: Applied Sciences, Vol 14, Iss 11, p 4916 (2024)
بيانات النشر: MDPI AG, 2024.
سنة النشر: 2024
المجموعة: LCC:Technology
LCC:Engineering (General). Civil engineering (General)
LCC:Biology (General)
LCC:Physics
LCC:Chemistry
مصطلحات موضوعية: non-uniform inflow, incident shock wave, transverse jet, X-51-like vehicle, Technology, Engineering (General). Civil engineering (General), TA1-2040, Biology (General), QH301-705.5, Physics, QC1-999, Chemistry, QD1-999
الوصف: During the operation of hypersonic vehicles, a reciprocal coupling effect is manifested between the inlet and the combustion chamber. This results in an unavoidable non-uniformity of conditions at the combustion chamber’s entrance, which, in turn, influences the fuel mixing within the chamber. The present study employed the Reynolds-averaged Navier–Stokes (RANS) equations to perform a numerical simulation of an X-51-like vehicle, with a focus on examining the impact of isolation section length and multi-injection strategies on the fuel mixing characteristics within the combustion chamber under conditions of non-uniform inflow. The findings indicated that a supersonic non-uniform inlet triggers incident shock waves, leading to a non-uniform pressure distribution across the flow section. Moreover, the position of injection was found to be pivotal in regulating penetration depth and mixing efficiency. The incident shock wave, bow shock, and boundary layer separation shock interacted with each other to increase local pressure. The coupling of high and low pressures generated an adverse pressure gradient that led to boundary layer separation, which further enhanced fuel penetration depth.
نوع الوثيقة: article
وصف الملف: electronic resource
اللغة: English
تدمد: 2076-3417
Relation: https://www.mdpi.com/2076-3417/14/11/4916; https://doaj.org/toc/2076-3417
DOI: 10.3390/app14114916
URL الوصول: https://doaj.org/article/8eb036b09ad142d9a48553b35b48fb1a
رقم الأكسشن: edsdoj.8eb036b09ad142d9a48553b35b48fb1a
قاعدة البيانات: Directory of Open Access Journals
الوصف
تدمد:20763417
DOI:10.3390/app14114916