Heat Transfer Analysis of Damaged Shrouded High-Pressure Turbine Rotor Blades

Due to the increasingly high turbine inlet temperatures, heat transfer analysis is now, more than ever, a vital part of the design and optimization of high-pressure turbine rotor blades of a modern jet engine. The present study aimed to find out how shape deviation and in-service deterioration affec...

Πλήρης περιγραφή

Λεπτομέρειες βιβλιογραφικής εγγραφής

Κύριοι συγγραφείς:	Mario Carta, Tiziano Ghisu, Shahrokh Shahpar
Μορφή:	Artigo
Γλώσσα:	Inglês
Έκδοση:	MDPI AG 2023-08-01
Σειρά:	International Journal of Turbomachinery, Propulsion and Power
Θέματα:	high-pressure turbine heat transfer shrouded blade level set meshing multi-fidelity simulation
Διαθέσιμο Online:	https://www.mdpi.com/2504-186X/8/3/24
Ετικέτες:	Προσθήκη ετικέτας Δεν υπάρχουν, Καταχωρήστε ετικέτα πρώτοι!