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

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...

Cur síos iomlán

Sonraí bibleagrafaíochta
Príomhchruthaitheoirí: Zhang, Q, O'Dowd, DO, He, L, Oldfield, M, Ligrani, P, ASME
Formáid: Conference item
Foilsithe / Cruthaithe: 2010