TRANSONIC TURBINE BLADE TIP AERO-THERMAL PERFORMANCE WITH DIFFERENT TIP GAPS: PART I - TIP HEAT TRANSFER

TRANSONIC TURBINE BLADE TIP AERO-THERMAL PERFORMANCE WITH DIFFERENT TIP GAPS: PART I - TIP HEAT TRANSFER

Show other versions (1)

A closely combined experimental and CFD study on a transonic blade tip aero-thermal performance at engine representative Mach and Reynolds numbers (Mexit=1, Reexit=1.27x106) is presented in this and its companion paper (Part II). The present paper considers surface heat transfer distributions on tip...

Descrición completa

Detalles Bibliográficos
Main Authors: Zhang, Q, O'Dowd, DO, He, L, Oldfield, M, Ligrani, P, ASME
Formato: Conference item
Publicado: 2010

Títulos similares

Títulos similares