Turbofan engine icing is a relatively new mode of icing attributed to solid phase ice accretion inside the engines. This occurs during flights at high altitudes through convective regions, where tiny ice crystals are ingested and make contact with the engine’s warm internal surfaces. The University of Southern Queensland has a small scale icing wind tunnel dedicated to studying aspects of thermal and particle conditions characteristic of ice accretion initiation in turbofan engines. This dissertation aimed to improve the operation of the facility’s refrigeration system by investigating the feasibility of implementing a steady flow work extraction device to super cool pressurised air via expansion processes. A DEPRAG rotary vane air mo...
This paper presents preliminary ice-crystal icing (ICI) altitude scaling evaluation results of a Hon...
This paper examines the aerodynamic design requirements of a cooled cooling air system for a large, ...
Ice accretion on external surfaces of aircraft is a widely recognised problem, but more recently ide...
Turbofan engine icing is a relatively new mode of icing attributed to solid phase ice accretion insi...
Numerous turbofan power loss events have occurred in high altitude locations in the presence of ice ...
It has been recognised in recent years that high altitude atmospheric ice crystals pose a threat to ...
The aviation industry has now connected a number of engine power-loss events to the ingestion of atm...
Thermal anti-icing systems are commonly used to protect aircraft leading edges from a potentially ha...
Due to numerous engine power-loss events associated with high-altitude convective weather, ice accre...
The Research Icing Wind Tunnel at the University of Southern Queensland (RIWT-USQ) has recently been...
Beyond its physical importance in both fundamental and climate research, atmospheric icing is consi...
There has been a substantial growth in the wind energy power capacity worldwide, and icing difficult...
This thesis gives a thorough description of the icing mechanisms in gas turbines, the underlying phy...
Core engine icing has been recognized to affect a wide variety of engines since the 1990's. This pre...
A significant number of historical engine powerloss events have recently been attributed to ingestio...
This paper presents preliminary ice-crystal icing (ICI) altitude scaling evaluation results of a Hon...
This paper examines the aerodynamic design requirements of a cooled cooling air system for a large, ...
Ice accretion on external surfaces of aircraft is a widely recognised problem, but more recently ide...
Turbofan engine icing is a relatively new mode of icing attributed to solid phase ice accretion insi...
Numerous turbofan power loss events have occurred in high altitude locations in the presence of ice ...
It has been recognised in recent years that high altitude atmospheric ice crystals pose a threat to ...
The aviation industry has now connected a number of engine power-loss events to the ingestion of atm...
Thermal anti-icing systems are commonly used to protect aircraft leading edges from a potentially ha...
Due to numerous engine power-loss events associated with high-altitude convective weather, ice accre...
The Research Icing Wind Tunnel at the University of Southern Queensland (RIWT-USQ) has recently been...
Beyond its physical importance in both fundamental and climate research, atmospheric icing is consi...
There has been a substantial growth in the wind energy power capacity worldwide, and icing difficult...
This thesis gives a thorough description of the icing mechanisms in gas turbines, the underlying phy...
Core engine icing has been recognized to affect a wide variety of engines since the 1990's. This pre...
A significant number of historical engine powerloss events have recently been attributed to ingestio...
This paper presents preliminary ice-crystal icing (ICI) altitude scaling evaluation results of a Hon...
This paper examines the aerodynamic design requirements of a cooled cooling air system for a large, ...
Ice accretion on external surfaces of aircraft is a widely recognised problem, but more recently ide...