Add to ORKGAn article presents a method for calculating the coordinates of a compressor blade profile based of circle
A very important catch, not only in the engineering, but also in any industry of production of natio...
The purpose of this paper is to present the advantages of the direct presCrIbed suRface Curvature di...
The blade geometry design method is an important tool to design high performance axial compressors, ...
The method for geometric modeling of the S-shaped camber line of the profile of an axial compressor ...
The paper presents the results of designing a compressor blade profile of type C4 using CAD, which i...
An article presents a new method for designing the turbo radial cascade based of blades - circles
AbstractIn the process of blade design, the shape of blade, which causes great influence on aerodyna...
Turbomachinery blade profiles in use today were all derived out of conventional methods. For example...
This paper presents the results of comparisons among some patented solutions for profiling the conto...
An article presents profiling turbine blades The computer program in Mathcad is an element of CAD de...
An article presents a method for designing a calculating plan for the turbine profiles with a fixed ...
Compressor blades are among the numerous and complicated parts of gas turbine engines. A freeform su...
This paper presents a method of general geometrical definitions of screw machine rotors and their ma...
The practice of designing centrifugal compressors in which impellers are the main components shows t...
This repository contains the source code used to generate compressor blade geometries for the follow...
A very important catch, not only in the engineering, but also in any industry of production of natio...
The purpose of this paper is to present the advantages of the direct presCrIbed suRface Curvature di...
The blade geometry design method is an important tool to design high performance axial compressors, ...
The method for geometric modeling of the S-shaped camber line of the profile of an axial compressor ...
The paper presents the results of designing a compressor blade profile of type C4 using CAD, which i...
An article presents a new method for designing the turbo radial cascade based of blades - circles
AbstractIn the process of blade design, the shape of blade, which causes great influence on aerodyna...
Turbomachinery blade profiles in use today were all derived out of conventional methods. For example...
This paper presents the results of comparisons among some patented solutions for profiling the conto...
An article presents profiling turbine blades The computer program in Mathcad is an element of CAD de...
An article presents a method for designing a calculating plan for the turbine profiles with a fixed ...
Compressor blades are among the numerous and complicated parts of gas turbine engines. A freeform su...
This paper presents a method of general geometrical definitions of screw machine rotors and their ma...
The practice of designing centrifugal compressors in which impellers are the main components shows t...
This repository contains the source code used to generate compressor blade geometries for the follow...
A very important catch, not only in the engineering, but also in any industry of production of natio...
The purpose of this paper is to present the advantages of the direct presCrIbed suRface Curvature di...
The blade geometry design method is an important tool to design high performance axial compressors, ...