A study of a large-scale model of an engine representative impingement cooling system has been performed. A series of tests were carried out to characterize the behavior of the system fully. These included cold flow diagnostic tests to determine the pressure loss and the static pressure distribution, and flow visualization to assess surface shear. The surface shear stress pattern provided by multiple stripes of colored paint applied to the target surface yielded important information on the near-wall flow features far from the jet axis. The row solved flow and pressure distributions are compared to industry standard predictions. Heat transfer tests using the transient liquid crystal technique were also conducted using coatings comprised of ...
AbstractA scaled up test model simulating a realistic leading edge cooling system of a high pressure...
This study examines experimentally the cooling performance of narrow impingement channels as could b...
As a key way of improving jet engine performance, a thermal tip clearance control system provides a ...
A study of a large-scale model of an engine representative impingement cooling system has been perfo...
Cast impingement cooling geometries offer the gas turbine designer higher structural integrity and i...
Cast impingement cooling geometries offer the gas turbine designer higher structural integrity and i...
In modern gas turbines parts of combustion chamber and turbine section are under heavy heat load, fo...
In modern gas turbines parts of combustion chamber and turbine section are under heavy heat load, fo...
This paper examines the applicability of a triple layer of thermochromic liquid crystals (TLCs) for ...
The inclusion of roughness elements on the target surface of a turbine aerofoil impingement cooling ...
The inclusion of roughness elements on the target surface of a turbine aerofoil impingement cooling ...
Impingement channels are often used in turbine blade cooling configurations. This paper examines the...
This research presents the possibility of the jet impingement cooling technique configuration for st...
Modern research on gas turbine cooling continues to focus on the optimization of different cooling d...
A heat transfer tunnel used for local convective heat transfer coefficient measurements on liquid cr...
AbstractA scaled up test model simulating a realistic leading edge cooling system of a high pressure...
This study examines experimentally the cooling performance of narrow impingement channels as could b...
As a key way of improving jet engine performance, a thermal tip clearance control system provides a ...
A study of a large-scale model of an engine representative impingement cooling system has been perfo...
Cast impingement cooling geometries offer the gas turbine designer higher structural integrity and i...
Cast impingement cooling geometries offer the gas turbine designer higher structural integrity and i...
In modern gas turbines parts of combustion chamber and turbine section are under heavy heat load, fo...
In modern gas turbines parts of combustion chamber and turbine section are under heavy heat load, fo...
This paper examines the applicability of a triple layer of thermochromic liquid crystals (TLCs) for ...
The inclusion of roughness elements on the target surface of a turbine aerofoil impingement cooling ...
The inclusion of roughness elements on the target surface of a turbine aerofoil impingement cooling ...
Impingement channels are often used in turbine blade cooling configurations. This paper examines the...
This research presents the possibility of the jet impingement cooling technique configuration for st...
Modern research on gas turbine cooling continues to focus on the optimization of different cooling d...
A heat transfer tunnel used for local convective heat transfer coefficient measurements on liquid cr...
AbstractA scaled up test model simulating a realistic leading edge cooling system of a high pressure...
This study examines experimentally the cooling performance of narrow impingement channels as could b...
As a key way of improving jet engine performance, a thermal tip clearance control system provides a ...