Experimental and theoretical analysis of carbon driven detonation waves in a heterogeneously premixed rotating detonation engine

IB Dunn, V Malik, W Flores, A Morales, KA Ahmed - Fuel, 2021 - Elsevier
Coal dust explosions can be hazardous; however, they can also generate a significant rise
in stagnation pressure if adequately harnessed. Rotating detonation combustors seek to …

[HTML][HTML] Thermal degradation of turbine components in a military turbofan

A Szczepankowski, R Przysowa - Engineering Failure Analysis, 2022 - Elsevier
In gas-turbine engines, temporary variation of the temperature field in the turbine inlet
causes thermal stress on the turbine components. In military engines, the afterburner is a …

Aircraft engine dust ingestion following sand storms

N Bojdo, A Filippone, B Parkes, R Clarkson - Aerospace Science and …, 2020 - Elsevier
Commercial aircraft operating in some regions of the world are subject to harsh atmospheric
conditions that can affect the efficiency and integrity of modern aero-engines. Conditions that …

Numerical research on vortex tube separator for special vehicle engine inlet air filter

T Dziubak, L Bąkała, M Karczewski… - Separation and …, 2020 - Elsevier
A two-stage inlet air filtration system used in the special vehicle combustion engine is
presented. A comparative analysis of the filtration properties of return and vortex tube …

Large eddy simulation of film cooling from cylindrical holes partially blocked by CaO-MgO-Al2O3-SiO2

X Chen, Y Long, Y Wang, S Weng, Y Luan - … Communications in Heat and …, 2021 - Elsevier
Abstract CaO-MgO-Al 2 O 3-SiO 2 (CMAS) melting and then sticking in the film cooling holes
is one of the important factors causing the cooling performance degradation of gas turbines …

Monte carlo predictions of aero-engine performance degradation due to particle ingestion

M Ellis, N Bojdo, A Filippone, R Clarkson - Aerospace, 2021 - mdpi.com
Aero-engines, which encounter clouds of airborne particulate, experience reduced
performance due to the deposition of particles on their high-pressure turbine nozzle guide …

Assessment of degradation equivalent operating time for aircraft gas turbine engines

O Alozie, YG Li, M Diakostefanis, X Wu… - The Aeronautical …, 2020 - cambridge.org
This paper presents a novel method for quantifying the effect of ambient, environmental and
operating conditions on the progression of degradation in aircraft gas turbines based on the …

Micron-sized particle transport and deposition in internal cooling duct with elliptical pin fins

J Liu, K Yu, C Peng, S Yao… - … of Engineering for …, 2023 - asmedigitalcollection.asme.org
The particle deposition in the internal cooling duct reduces the heat transfer efficiency,
increases the instability of aero-engine operation, and brings serious challenges to the …

Binary collision of CMAS droplets—Part I: Equal-sized droplets

H Ganti, P Khare, L Bravo - Journal of Materials Research, 2020 - cambridge.org
This study focuses on binary droplet collisions of equal calcium–magnesium–
aluminosilicate (CMAS) droplets formed by the melting of dust and sand ingested by gas …

Dust adhesion and deposition behavior in internal cooling duct with pin fins

J Liu, K Yu, D Tafti, X Yang, H Xu - International Journal of Thermal …, 2023 - Elsevier
The collision-adhesion and deposition of micron-sized dust particles in the internal cooling
duct with pin fin arrays are investigated, integrating the energy dissipation collision model of …