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Author : Richard F. Soltis,Donald C. Urasek,Max Joseph Miller
Publisher : Unknown
Page : 44 pages
File Size : 48,5 Mb
Release : 1969
Category : Centrifugal pumps
ISBN : UIUC:30112106877183
Blade element performance of tandem bladed inducer tested in water.
Author : Richard F. Soltis
Publisher : Unknown
Page : 42 pages
File Size : 48,9 Mb
Release : 1969
Category : Centrifugal pumps
ISBN : UIUC:30112101602941
Author : Anonim
Publisher : Unknown
Page : 332 pages
File Size : 41,9 Mb
Release : 1969
Category : Electronic
ISBN : MINN:319510008462637
Author : Anonim
Publisher : Unknown
Page : 1282 pages
File Size : 41,7 Mb
Release : 1982
Category : Aeronautics
ISBN : UIUC:30112102359566
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1348 pages
File Size : 54,7 Mb
Release : 1970
Category : United States
ISBN : STANFORD:36105019598304
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1320 pages
File Size : 40,7 Mb
Release : 1966
Category : Government publications
ISBN : WISC:89035089036
Author : Anonim
Publisher : Unknown
Page : 1730 pages
File Size : 42,8 Mb
Release : 1970
Category : Government publications
ISBN : UOM:39015022681913
Author : Anonim
Publisher : Unknown
Page : 772 pages
File Size : 49,5 Mb
Release : 1970
Category : Mechanics, Applied
ISBN : UCAL:C2682439
Author : Anonim
Publisher : Unknown
Page : 212 pages
File Size : 49,6 Mb
Release : 1970
Category : Science
ISBN : UIUC:30112101038138
Author : George K. Serovy
Publisher : Unknown
Page : 258 pages
File Size : 45,8 Mb
Release : 1973
Category : Pumping machinery
ISBN : UIUC:30112106629808
Author : James E. Crouse
Publisher : Unknown
Page : 76 pages
File Size : 50,7 Mb
Release : 1967
Category : Axial flow compressors
ISBN : UIUC:30112106869826
Author : A. Poncet,B. Lakshminarayana
Publisher : Unknown
Page : 140 pages
File Size : 53,7 Mb
Release : 1973
Category : Pumping machinery
ISBN : UIUC:30112106628115
Because of the long and narrow passages between the blades of a rocket pump inducer, major effects from turbulence and viscosity make the flow through such a device truly three-dimensional and therefore difficult to measure or predict. To investigate the flow characteristics, conventional and three-dimensional hot-wire probe measurements were conducted in a model inducer 3 ft in diameter. Blade-to-blade variation of the three components of velocity at the exit and the corresponding turbulence intensities were obtained by means of hotwire probes aligned in the three coordinate directions. Analysis of the three-dimensional inviscid flow field led to qualitative prediction of the flow characteristics. Extensive measurements and theoretical analyses of the flow field showed that blade blockage, viscosity, and blade boundary layer interactions are the dominant influences on flow in this type of turbomachinery.
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher : Unknown
Page : 428 pages
File Size : 48,6 Mb
Release : 1968
Category : Aeronautics
ISBN : STANFORD:36105024415957
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher : Unknown
Page : 436 pages
File Size : 49,5 Mb
Release : 1968
Category : Aeronautics
ISBN : CORNELL:31924057848842
Author : C. A. Gorton
Publisher : Unknown
Page : 194 pages
File Size : 54,9 Mb
Release : 1980
Category : Turbomachines
ISBN : NASA:31769000504467
