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Three Dimensional Simulation of Supersonic Flow over Missiles of Different Shapes
تمثيل ثلاثي الابعاد لمجرى فوق الصوتي لمقذوفات ذات اشكال مختلفة

Authors: Jalal M. Jalil --- Hussain H. Al-Kayiem --- Ahmed Kadhim Hussein
Journal: Engineering and Technology Journal مجلة الهندسة والتكنولوجيا ISSN: 16816900 24120758 Year: 2012 Volume: 30 Issue: 3 Pages: 325-343
Publisher: University of Technology الجامعة التكنولوجية

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Abstract

In this work, a three-dimensional primitive variable of supersonic flow overmissiles was computed based on finite difference computational fluid dynamicmethods. The problem was considered is to deal with external, inviscid, compressiblesupersonic- flow over three-dimensional missiles with and without canard. Eulerequations were solved using time-marching MacCormack’s explicit technique. Theflow conditions are taken at sea level and Mach number was tested up to 4.0. To dealwith complex shape of missiles the so-called “body fitted coordinate system” wasconsidered and the algebraic and elliptic methods were used to generate grids overmissiles. The number of iterations and the number of mesh points depending onMach number. The result indicate, that for the same Mach number, the increasing ofmesh points, lead to increase of the number of iterations

في هذا البحث, حسب الجريان فوق الصوتي الثلاثي البعدعبر مقذوفات بطريقة الفروقات المحددةلديناميك الموائع الحسابي. لقد اعتبرت المسألة ذات جريان خارجي فوق صوتي لاأنضغاطيغيرلذج عبر مقذوفات ثلاثية البعد مع كنرد تقليدي وبدون كنرد. حلت معادلات أويلرباستخدام تكنيكمكورمك الظاهرمع الوقت. ظروف الجريان أخذت عند مستوى سطح البحر مع عدد ماخ لغاية 2.5للتعامل مع الشكل المعقد للمقذوفات, استخدمت نظام احداثيات مطابقة الجسم بالطرق الجبريةوالبيضوية لتوليد الشبكة عبر المقذوفات. اظهرت النتائج تطابق جيد مع النتائج المنشورة.


Article
Transient Buoyancy- Driven Laminar Convection in an Inclined Three- Dimensional Trapezoidal Enclosure

Authors: Ahmed Kadhim Hussein --- Kolsi Lioua --- Hussain H. Al-Kayiem
Journal: Basrah Journal for Engineering Science مجلة البصرة للعلوم الهندسية ISSN: Print: 18146120; Online: 23118385 Year: 2014 Volume: 14 Issue: 2 Pages: 216-228
Publisher: Basrah University جامعة البصرة

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Abstract

Numerical analysis of transient laminar threedimensionalbuoyancy-driven convection in an inclined threedimensionaltrapezoidal air-filled enclosure was investigated inthis paper. The right and left sidewalls of the enclosure arekept at constant cold temperatures. The bottom wall ismaintained at a constant hot temperature , while the top wall isconsidered adiabatic. Numerical investigation is performed forRayleigh numbers varied as 103 ≤ Ra ≤ 105 , while thetrapezoidal enclosure inclination angle is varied as 0° ≤  ≤180°. Prandtl number is considered constant at Pr = 0.71. Flowand thermal fields are presented in both two and threedimensionalpattern. Also, both local and average Nusseltnumbers are calculated and discussed. The results show thatwhen the Rayleigh number increases, the flow patterns arechanged especially in three-dimensional results and the flowcirculation increases. The minimum average Nusselt numberinside the trapezoidal cavity corresponds to the highestinclination angle [i.e., 180 ].While, the average Nusseltnumber reaches its maximum value at    30 . Moreover,when the Rayleigh number increases the average Nusseltnumber increases as expected.

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