Author:
Kozul Melissa,Nardini Massimiliano,Sandberg R. D.
Reference22 articles.
1. M. Thomas Combustor-turbine interactions: Hot spot migration and thermal environment prediction for a better understanding and design of helicopter engines. Doctoral Thesis, CERFACS, 2021
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3. T. Bacci, A. Picchi, G. Babazzi, B. Facchini and S. Cubeda Heat transfer coefficient and adiabatic wall temperature measurements on a high-pressure turbine nozzle guide vanes with representative inlet swirl and temperature distortions Proc. ASME Turbo Expo, GT2022-81263, 2022
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