مشروع البحث:
The effect of air lnlet to gas turbine combustion chamber on flame stability and temperatures distribution

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المساهمين
الممولين
رقم التعريف
5682
الباحث
سعد عبدالسلام تكاله
المشرفين
منشورات
وحدات تنظيمية
الوصف
The experimental results show a significant effect of secondary air swirl and swirl strength on flame stability, and temperatures distributions. On the other hand the low temperatures are recorded at the wall along the combustor, and a significant temperatures distributions at exit of the combustion chamber.
الكلمات الدالة
air inlet into Gas Turbine combustion chamber