The results of gas current calculations in a flow part in not reversive jet-reactive turbine at pressure upon an input to the turbine up to 10 МPа (earlier calculations were spent up to 0.9 МPа), executed in program complex FlowVision for the first time are presented in the article. The dependences of factors and parameters of efficiency of the jet-reactive turbine (JRT) from total pressure upon an input in the turbine are received. They are exposed in a graphic type. The primary goals of the research were: calculation of parameters of current of gas in a flow part of the jet-reactive turbine by means of program complex FlowVision at pressure upon an input of the JRT from 0.4 up to 10 МPа, the analysis of results of calculation, reception o...
In the thermodynamic design of turbines and compressor's it is essential firstly to decide on the ba...
Gas-turbines are widely used to power aero planes because they are light, compact with a high power-...
The design and adjustment of modern gas turbine engines significantly rely on the use of numerical r...
Efficiency tests have been conducted on a single-stage impulse turbine having a 13.2-inch pitch-line...
An investigation has been made of the effect on the performance of a radial-flow exhaust-gas turbosu...
A gas turbine installation (GTI) consists of 5 main parts: an input device, a compressor, a combusti...
One of the promising trends to increase the fuel and energy efficiency of gas turbines is contact co...
The article deals with the working processes in flowing part of the turbo-compressors with general i...
The performance of the turbine component of a J33 turbojet engine was determined over a range of tur...
Current progress in gas turbine performance is achieved mainly by increasing the turbine inlet tempe...
Over the last decade, aircraft gas turbine engines have achieved a high degree of excellence and rel...
The design and adjustment of modern gas turbine engines significantly rely on the use of numerical r...
The engine manufacturers adopt new measures in order to further improve the characteristics of a tur...
A two-phase hydraulic turbine’s performance and flow field were predicted under different Inlet Gas ...
The article presents reasons for generating a non-uniform field of parameters in the compressor inle...
In the thermodynamic design of turbines and compressor's it is essential firstly to decide on the ba...
Gas-turbines are widely used to power aero planes because they are light, compact with a high power-...
The design and adjustment of modern gas turbine engines significantly rely on the use of numerical r...
Efficiency tests have been conducted on a single-stage impulse turbine having a 13.2-inch pitch-line...
An investigation has been made of the effect on the performance of a radial-flow exhaust-gas turbosu...
A gas turbine installation (GTI) consists of 5 main parts: an input device, a compressor, a combusti...
One of the promising trends to increase the fuel and energy efficiency of gas turbines is contact co...
The article deals with the working processes in flowing part of the turbo-compressors with general i...
The performance of the turbine component of a J33 turbojet engine was determined over a range of tur...
Current progress in gas turbine performance is achieved mainly by increasing the turbine inlet tempe...
Over the last decade, aircraft gas turbine engines have achieved a high degree of excellence and rel...
The design and adjustment of modern gas turbine engines significantly rely on the use of numerical r...
The engine manufacturers adopt new measures in order to further improve the characteristics of a tur...
A two-phase hydraulic turbine’s performance and flow field were predicted under different Inlet Gas ...
The article presents reasons for generating a non-uniform field of parameters in the compressor inle...
In the thermodynamic design of turbines and compressor's it is essential firstly to decide on the ba...
Gas-turbines are widely used to power aero planes because they are light, compact with a high power-...
The design and adjustment of modern gas turbine engines significantly rely on the use of numerical r...