Analytical Determination of Radial Inflow Turbine Design Geometry for Maximum Efficiency
Author : Harold E. Rohlik
Publisher :
Page : 38 pages
File Size : 31,64 MB
Release : 1968
Category : Turbines
ISBN :
Author : Harold E. Rohlik
Publisher :
Page : 38 pages
File Size : 31,64 MB
Release : 1968
Category : Turbines
ISBN :
Author : S. Larry Dixon
Publisher : Elsevier
Page : 414 pages
File Size : 18,27 MB
Release : 2005-03-30
Category : Science
ISBN : 0080470629
The new edition will continue to be of use to engineers in industry and technological establishments, especially as brief reviews are included on many important aspects of Turbomachinery, giving pointers towards more advanced sources of information. For readers looking towards the wider reaches of the subject area, very useful additional reading is referenced in the bibliography. The subject of Turbomachinery is in continual review, and while the basics do not change, research can lead to refinements in popular methods, and new data can emerge. This book has applications for professionals and students in many subsets of the mechanical engineering discipline, with carryover into thermal sciences; which include fluid mechanics, combustion and heat transfer; dynamics and vibrations, as well as structural mechanics and materials engineering. - An important, long overdue new chapter on Wind Turbines, with a focus on blade aerodynamics, with useful worked examples - Includes important material on axial flow compressors and pumps - Example questions and answers throughout
Author : Michael R. Galvas
Publisher :
Page : 44 pages
File Size : 16,49 MB
Release : 1972
Category : Compressors
ISBN :
Centrifugal compressor performance was examined analytically to determine optimum geometry for various applications as characterized by specific speed. Seven specific losses were calculated for various combinations of inlet tip-exit diameter ratio, inlet hub-tip diameter ratio, blade exit backsweep, and inlet-tip absolute tangential velocity for solid body prewhirl. The losses considered were inlet guide vane loss, blade loading loss, skin friction loss, recirculation loss, disk friction loss, vaneless diffuser loss, and vaned diffuser loss. Maximum total efficiencies ranged from 0.497 to 0.868 for a specific speed range of 0.257 to 1.346. Curves of rotor exit absolute flow angle, inlet tip-exit diameter ratio, inlet hub-tip diameter ratio, head coefficient and blade exit backsweep are presented over a range of specific speeds for various inducer tip speeds to permit rapid selection of optimum compressor size and shape for a variety of applications.
Author : Earl Logan, Jr.
Publisher : CRC Press
Page : 280 pages
File Size : 32,77 MB
Release : 2013-12-19
Category : Science
ISBN : 1482247844
"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 a
Author : United States. Superintendent of Documents
Publisher :
Page : 1348 pages
File Size : 45,56 MB
Release : 1970
Category : United States
ISBN :
Author :
Publisher :
Page : 1386 pages
File Size : 48,78 MB
Release :
Category : Government publications
ISBN :
Author : Sandra K. Faull
Publisher : Arlington, Va. : United States Historical Documents Institute
Page : 608 pages
File Size : 21,52 MB
Release : 1979
Category : Reference
ISBN :
Author :
Publisher :
Page : 540 pages
File Size : 13,87 MB
Release : 1976
Category :
ISBN :
Author : Arthur J. Glassman
Publisher :
Page : 70 pages
File Size : 43,34 MB
Release : 1976
Category : Turbines
ISBN :
Author :
Publisher :
Page : 936 pages
File Size : 50,78 MB
Release : 1977
Category : Aeronautics
ISBN :