Computer Program for Design Analysis of Radial-inflow Turbines PDF Download
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Author: Arthur J. Glassman
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 70
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Book Description
Author: Arthur J. Glassman
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 70
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Book Description
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781724266552
Category :
Languages : en
Pages : 28
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Book Description
The analysis procedure of an existing computer program was extended to include rotor blade sweep, to model the flow more accurately at the rotor exit, and to provide more detail to the loss model. The modeling changes are described and all analysis equations and procedures are presented. Program input and output are described and are illustrated by an example problem. Results obtained from this program and from a previous program are compared with experimental data. Meitner, P. L. and Glassman, A. J. Glenn Research Center NASA-TP-2199, NAS 1.60:2199, AVRADCOM-TR-83-C-4 RTOP 535-05-12
Author: Earl Logan, Jr.
Publisher: CRC Press
ISBN: 9780824791384
Category : Science
Languages : en
Pages : 286
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Book Description
"This entirely updated and enlarged Second Edition broadens the scope of the previous edition while maintaining its concise, easy-to-read style in presenting the basic principles of turbomachine theory and its application to specific devices -- providing immediately useful step-by-step procedures that show how the essentials of turbomachinery are applied in design and to predict performance. "
Author: D. G. Wilson
Publisher:
ISBN:
Category :
Languages : en
Pages : 437
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Book Description
Author: Peter L. Meitner
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 32
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Book Description
The analysis procedure of an existing computer program was extended to include rotor blade sweep, to model the flow more accurately at the rotor exit, and to provide more detail to the loss model. This report describes the modeling changes and presents all analysis equations and procedures. Program input and output are described and are illustrated by an example problem. Results obtained from this program and from a previous program are compared with experimental data. (Author).
Author: Peter L. Meitner
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 32
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 540
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Book Description
Author: Charles A. Wasserbauer
Publisher:
ISBN:
Category : FORTRAN (Computer program language)
Languages : en
Pages : 60
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Book Description
Author: Arthur J. Glassman
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 44
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Book Description
The program method is based on a mean-diameter flow analysis. Input design requirements include power or pressure ratio, flow, temperature, pressure, and speed. Turbine designs are generated for any specified number of stages and for any of three types of velocity diagrams (symmetrical, zero exit swirl, or impulse). Exit turning vanes can be included in the design. Program output includes inlet and exit annulus dimensions, exit temperature and pressure, total and static efficiencies, blading angles, and last-stage critical velocity ratios. The report presents the analysis method, a description of input and output with sample cases, and the program listing.
Author: Carroll A. Todd
Publisher:
ISBN:
Category : FORTRAN IV (Computer program language)
Languages : en
Pages : 60
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Book Description
