Add to ORKGProgram uses one-dimensional mean streamline analysis conducted at fixed stagnation conditions. Seven specific losses are calculated for each set of compressors geometric variables and inlet velocity diagram characteristics studied. Categories used as input information are compressor geometry, thermodynamic properties of working fluid, velocity diagram characteristics, and iteration limits
TutorialThis tutorial will provide several examples of how a users specified conditions impact the s...
This paper describes a method to estimate key aerodynamic parameters of single and multi-stage axial...
This paper describes the construction of the centrifugal compressor model and its validation with th...
A computer program for predicting design point specific speed - efficiency characteristics of centri...
Centrifugal compressor performance was examined analytically to determine optimum geometry for vario...
A FORTRAN program for calculating the off-design performance of centrifugal compressors with channel...
The program will determine the velocities in the meridional plane of a backward-swept impeller, a ra...
Decades ago at pre – computer era design process consisted of empirically based set of rules applica...
A centrifugal compressor, which is driven by a gas turbine, is one of the critical equipment used i...
LecturePg. 35-42Facing increased market demands for improved aerodynamic efficiency, centrifugal com...
Overall performance of 6-inch radial-bladed centrifugal compressor with various diffuser vane settin...
The measured aerodynamic performance of a compact, high work-factor, single-stage centrifugal compre...
A centrifugal compressor was designed for a gas turbine powered automobile as part of the Energy Res...
Computer program calculates the velocity distribution and streamlines over widely separated blades o...
A centrifugal compressor facility being built by the NASA Lewis Research Center is described; its pu...
TutorialThis tutorial will provide several examples of how a users specified conditions impact the s...
This paper describes a method to estimate key aerodynamic parameters of single and multi-stage axial...
This paper describes the construction of the centrifugal compressor model and its validation with th...
A computer program for predicting design point specific speed - efficiency characteristics of centri...
Centrifugal compressor performance was examined analytically to determine optimum geometry for vario...
A FORTRAN program for calculating the off-design performance of centrifugal compressors with channel...
The program will determine the velocities in the meridional plane of a backward-swept impeller, a ra...
Decades ago at pre – computer era design process consisted of empirically based set of rules applica...
A centrifugal compressor, which is driven by a gas turbine, is one of the critical equipment used i...
LecturePg. 35-42Facing increased market demands for improved aerodynamic efficiency, centrifugal com...
Overall performance of 6-inch radial-bladed centrifugal compressor with various diffuser vane settin...
The measured aerodynamic performance of a compact, high work-factor, single-stage centrifugal compre...
A centrifugal compressor was designed for a gas turbine powered automobile as part of the Energy Res...
Computer program calculates the velocity distribution and streamlines over widely separated blades o...
A centrifugal compressor facility being built by the NASA Lewis Research Center is described; its pu...
TutorialThis tutorial will provide several examples of how a users specified conditions impact the s...
This paper describes a method to estimate key aerodynamic parameters of single and multi-stage axial...
This paper describes the construction of the centrifugal compressor model and its validation with th...