Add to ORKGA methodology based on geometric construction of CDA profiles and CFD flow simulation has been used to design a stator blade of a 3-stage LP compressor. The designed CDA blade is shown to13; perform better in terms of efficiency, pressure ratio and stall margin of the compressor compared to the original MCA blade
Pratt & Whitney Aircraft is conducting a test program for NASA in order to demonstrate that a contro...
One of the most prominent trends in the development of axial compressors during the last decades was...
The basic tool set to design multi-stage axial compressors consists of fast codes for throughflow an...
A methodology based on geometric construction of CDA profiles and CFD flow simulation has been used ...
With an aim to improve the performance of a multistage LP compressor, one of the stator blades has b...
This paper describes the design and performance evaluation of a controlled diffusion aerofoil (CDA) ...
A second generation, highly loaded stator having controlled diffusion airfoil (CDA) sections with en...
The objective of the presented work is to perform numerical and experimental studies on compressor s...
International Gas Turbine Conference and Exhibit; 8-12 Jun. 1986; Dusseldorf; GermanyThe mid-span se...
International audienceThis paper describes a new design method for high Reynolds number subsonic com...
The conventional methods for the design of the blades in the case of axial turbomachines are conside...
Ensuring a high degree of commonality among a range of products can dramatically decrease developmen...
The purpose of this research was to develop a searchable, expandable database of compressor blade pr...
The pursuit of efficient, compact and lightweight aircraft engines are important as it leads to a re...
Aircraft are incontestably an important way of transportation in our society, for both commercial an...
Pratt & Whitney Aircraft is conducting a test program for NASA in order to demonstrate that a contro...
One of the most prominent trends in the development of axial compressors during the last decades was...
The basic tool set to design multi-stage axial compressors consists of fast codes for throughflow an...
A methodology based on geometric construction of CDA profiles and CFD flow simulation has been used ...
With an aim to improve the performance of a multistage LP compressor, one of the stator blades has b...
This paper describes the design and performance evaluation of a controlled diffusion aerofoil (CDA) ...
A second generation, highly loaded stator having controlled diffusion airfoil (CDA) sections with en...
The objective of the presented work is to perform numerical and experimental studies on compressor s...
International Gas Turbine Conference and Exhibit; 8-12 Jun. 1986; Dusseldorf; GermanyThe mid-span se...
International audienceThis paper describes a new design method for high Reynolds number subsonic com...
The conventional methods for the design of the blades in the case of axial turbomachines are conside...
Ensuring a high degree of commonality among a range of products can dramatically decrease developmen...
The purpose of this research was to develop a searchable, expandable database of compressor blade pr...
The pursuit of efficient, compact and lightweight aircraft engines are important as it leads to a re...
Aircraft are incontestably an important way of transportation in our society, for both commercial an...
Pratt & Whitney Aircraft is conducting a test program for NASA in order to demonstrate that a contro...
One of the most prominent trends in the development of axial compressors during the last decades was...
The basic tool set to design multi-stage axial compressors consists of fast codes for throughflow an...