This report describes the computer aided design of centrifugal impellers using microprocessor based HP 98365 desktop computer. For a specified parameters of mass flow note and pressure ratio, this software designs an optimum aerodynamic configuration of the centrifugal impeller. It also generates the isometric and other geometrical views along with the surface co-ordinates for matching process. To demonstrate this software, a high pressure ratio centrifugal impeller was considered. The aerodynamic design and the generation of geometrical views for the above impeller were discussed in detail
A computer program is reported for the integrated design of centrifugal fan and blower impellers and...
Combined numerical simulation with experiment, blade wrap angle, and blade exit angle are varied to ...
The problem of this paper is aerodynamic design of 8:1 pressure ratio centrifugal compressor possess...
This report describes the computer aided design of centrifugal impellers using microprocessor based ...
This report describes the Computer Aided Design of Centrifugal Impellers using microprocessor based ...
This report describes the Computer Aided Design of Centrifugal Impellers using microprocessor based ...
This report describes the aerodynamic design of centrifugal compressors.The design approach is based...
This report describes the aerodynamic design of centrifugal compressors.The design approach is based...
A procedure is described to design the overall dimensions of a centrifugal impeller. Initial optimiz...
This thesis deals with centrifugal pump impeller design for given parameters. This pump impeller des...
The design of centrihgal pump involves a large number of empirical data derived from experimental ev...
A general purpose design methodology for high pressure ratio centrifugal compressor was developed.Th...
The practice of designing centrifugal compressors in which impellers are the main components shows t...
AbstractFor the past two years, Mechanical & Aerospace Engineering students at the University of Flo...
Combined numerical simulation with experiment, blade wrap angle, and blade exit angle are varied to ...
A computer program is reported for the integrated design of centrifugal fan and blower impellers and...
Combined numerical simulation with experiment, blade wrap angle, and blade exit angle are varied to ...
The problem of this paper is aerodynamic design of 8:1 pressure ratio centrifugal compressor possess...
This report describes the computer aided design of centrifugal impellers using microprocessor based ...
This report describes the Computer Aided Design of Centrifugal Impellers using microprocessor based ...
This report describes the Computer Aided Design of Centrifugal Impellers using microprocessor based ...
This report describes the aerodynamic design of centrifugal compressors.The design approach is based...
This report describes the aerodynamic design of centrifugal compressors.The design approach is based...
A procedure is described to design the overall dimensions of a centrifugal impeller. Initial optimiz...
This thesis deals with centrifugal pump impeller design for given parameters. This pump impeller des...
The design of centrihgal pump involves a large number of empirical data derived from experimental ev...
A general purpose design methodology for high pressure ratio centrifugal compressor was developed.Th...
The practice of designing centrifugal compressors in which impellers are the main components shows t...
AbstractFor the past two years, Mechanical & Aerospace Engineering students at the University of Flo...
Combined numerical simulation with experiment, blade wrap angle, and blade exit angle are varied to ...
A computer program is reported for the integrated design of centrifugal fan and blower impellers and...
Combined numerical simulation with experiment, blade wrap angle, and blade exit angle are varied to ...
The problem of this paper is aerodynamic design of 8:1 pressure ratio centrifugal compressor possess...