Fluid Dynamics & Materials Processing2026，Vol.22Issue(6)：P.106-136,31.DOI:10.32604/fdmp.2026.082520
A Combined Asymptotic and Characteristic-Based Computational Framework for Exit-Plane Disturbance Response in Solid Rocket Motor Chambers
Abdelkarim Hegab 1Faisal Albatati 1Ahmad Hussain 2Asad A.Zaidi 3Abdullah Abuhabaya 1Ragab A.El-Sehiemy4
作者信息
- 1. Mechanical Engineering Department,Faculty of Engineering,King Abdulaziz University,Rabigh,Saudi Arabia
- 2. Department of Mechanical Engineering,DHA Suffa University,Karachi,Pakistan
- 3. Department of Mechanical Engineering,Faculty of Engineering,Islamic University of Madinah,Madinah,Saudi Arabia
- 4. Electrical Engineering Department,Faculty of Engineering,Kafrelshiekh University,Kafr El-Sheikh,Egypt Széchenyi István University,Egyetem tér 1.,Győr,Hungary
- 折叠
摘要
关键词
Solid rocket motor/aeroacoustics/computational fluid dynamics/characteristic boundary conditions/acoustic-vorticity interaction/Reynolds-number effects/exit-plane forcing/unsteady compressible flow分类
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Abdelkarim Hegab,Faisal Albatati,Ahmad Hussain,Asad A.Zaidi,Abdullah Abuhabaya,Ragab A.El-Sehiemy..A Combined Asymptotic and Characteristic-Based Computational Framework for Exit-Plane Disturbance Response in Solid Rocket Motor Chambers[J].Fluid Dynamics & Materials Processing,2026,22(6):P.106-136,31.
