Gas turbine engine efficiency and reliability is generally improved through better understanding and improvements to the design of individual components. The life limiting component of the modern gas turbine is the high pressure (HP) turbine stage due to the arduous environment. Over the last 50 years significant research effort has been focused on advancing blade cooling designs and materials. Due to practical limitations little fundamental research on the turbine system is performed in the operating gas turbine engine. Consequently different types of experimental approaches have been developed over the last 4 decades to study the flow and in particular the heat transfer and cooling in turbines. In general the facilities can be divided int...
Gas turbines have applications in jet engine propulsion and energy-generation for land-based systems...
Increases in power density and thermal efficiency of a highly efficient gas turbine engine motivate ...
An assessment of the performance and operating attributes of a high-speed small gas turbine engine w...
Cooling is essential in all modern high-temperature gas turbines. Turbine cooling is mainly a functi...
The turbine blade cooling has been considered to be a unique solution to increase the efficiency of ...
The present paper deals with the experimental aero-heat transfer studies performed in rotating turbi...
There is an everlasting demand for higher cycle efficiencies in gas turbine engines. One way to obta...
In today’s industrial scenario, Gas Turbine is one of the most important components of auxiliary pow...
Performance of a gas turbine is mainly depends on various parameters e.g. ambient temperature, compr...
The engine manufacturers adopt new measures in order to further improve the characteristics of a tur...
In this thesis, novel cooling systems for gas turbine blade platforms were developed and assessed ex...
This paper describes a new modular experimental facility that was purpose-built to investigate flow ...
The first part of the paper presents commissioning of a single-stage high-pressure (HP) turbine empl...
The European gas turbine industry faces unremitting competitive pressure from the USA and the Far Ea...
Unsteady three-dimensional flow phenomena have major effects on the aerodynamic performance of, and ...
Gas turbines have applications in jet engine propulsion and energy-generation for land-based systems...
Increases in power density and thermal efficiency of a highly efficient gas turbine engine motivate ...
An assessment of the performance and operating attributes of a high-speed small gas turbine engine w...
Cooling is essential in all modern high-temperature gas turbines. Turbine cooling is mainly a functi...
The turbine blade cooling has been considered to be a unique solution to increase the efficiency of ...
The present paper deals with the experimental aero-heat transfer studies performed in rotating turbi...
There is an everlasting demand for higher cycle efficiencies in gas turbine engines. One way to obta...
In today’s industrial scenario, Gas Turbine is one of the most important components of auxiliary pow...
Performance of a gas turbine is mainly depends on various parameters e.g. ambient temperature, compr...
The engine manufacturers adopt new measures in order to further improve the characteristics of a tur...
In this thesis, novel cooling systems for gas turbine blade platforms were developed and assessed ex...
This paper describes a new modular experimental facility that was purpose-built to investigate flow ...
The first part of the paper presents commissioning of a single-stage high-pressure (HP) turbine empl...
The European gas turbine industry faces unremitting competitive pressure from the USA and the Far Ea...
Unsteady three-dimensional flow phenomena have major effects on the aerodynamic performance of, and ...
Gas turbines have applications in jet engine propulsion and energy-generation for land-based systems...
Increases in power density and thermal efficiency of a highly efficient gas turbine engine motivate ...
An assessment of the performance and operating attributes of a high-speed small gas turbine engine w...