Cracking analysis of an aero-engine combustor

Gas turbine coatings – An overview

R. Rajendran · Engineering Failure Analysis · 2012 · 319 citations

Engineering, Materials Engineering, Materials Science +12

Degradation study of 7 wt.% yttria stabilised zirconia (7YSZ) thermal barrier coatings on aero-engine combustion chamber parts due to infiltration by different CaO–MgO–Al 2 O 3 –SiO 2 variants

Ravisankar Naraparaju, Uwe Schulz, Peter Mechnich et al. · Surface and Coatings Technology · 2014 · 77 citations

Natural Sciences, Materials Engineering, Materials Science +17

LES of a Multi-burner Annular Gas Turbine Combustor

Christer Fureby · Flow Turbulence and Combustion · 2009 · 66 citations

Engineering, Aerospace Engineering, Mechanical Engineering +12

The effect of effusion holes inclination angle on the adiabatic film cooling effectiveness in a three-sector gas turbine combustor rig with a realistic swirling flow

Antonio Andreini, Riccardo Becchi, Bruno Facchini et al. · International Journal of Thermal Sciences · 2017 · 63 citations · Full text

Engineering, Mechanical Engineering, Physics +16

Time-resolved study of transient soot formation in an aero-engine model combustor at elevated pressure

Michael Stöhr, Klaus Peter Geigle, Redjem Hadef et al. · Proceedings of the Combustion Institute · 2018 · 44 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17