The effect of hot-streaks on HP vane surface and endwall heat transfer: An experimental and numerical study

Pronounced non-uniformities in combustor exit flow temperature (hot-streaks), which arise because of discrete injection of fuel and dilution air jets within the combustor and because of end-wall cooling flows, affect both component life and aerodynamics. Because it is very difficult to quantitativel...

Täydet tiedot

Bibliografiset tiedot
Päätekijät: Povey, T, Chana, K, Jones, T, Hurrion, J
Aineistotyyppi: Journal article
Kieli:English
Julkaistu: 2007