طيار مهندس/ محمد الشعلان، نويليا نونيز، ساشين ناجاراجا، فرانسيسكو لوبيز
المؤلفون بالإنجليزي
Mehmed asch-Schaalan, Noelia Nunez, Sachin Nagaraja, Francisco Lopez
الملخص الانجليزي
This measurement will deep dive into two elements of the high pressure body of the DGEN 380, the centrifugal compressor and the axial turbine, as well as in other fundamental components such as bearings and the lubrication system. Further reasoning with regards to energy transfer, temperature evolution, entropy and degree of reaction will be issued. Finally, the material selection for the compressor and turbine will explored.
طيار مهندس/ محمد الشعلان | Capt. Mehmed asch-Schaalan | 5640