Experimental Investigation of the effects of a modern lean burn combustor outflow on the performance of a film-cooled NGV cascade. Evaluation of chamber flow field, NGV inlet/outlet aerothermal field, turbulence decay and adiabatic effectiveness on the NGV profiles
Experimental investigation on a high pressure NGV cascade in the presence of a representative lean burn aero-engine combustor outflow
2018
Abstract
Experimental Investigation of the effects of a modern lean burn combustor outflow on the performance of a film-cooled NGV cascade. Evaluation of chamber flow field, NGV inlet/outlet aerothermal field, turbulence decay and adiabatic effectiveness on the NGV profilesFile in questo prodotto:
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https://hdl.handle.net/20.500.14242/132298
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URN:NBN:IT:UNIFI-132298