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Author : Karl Kovach
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.3/5 (91 download)
Download or read book Investigation of Effects of Reynolds Number on Large Double-entry Centrifugal Compressor written by Karl Kovach and published by . This book was released on 1952 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Laurence J. Heidelberg
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Effect of Reynolds Number on Overall Performance of a 6-inch Radial Bladed Centrifugal Compressor written by Laurence J. Heidelberg and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Gilbert K. Sievers
Publisher :
ISBN 13 :
Total Pages : 21 pages
Book Rating : 4.:/5 (715 download)
Download or read book Investigation of Reynolds Number Effect on Performance of an Eight-stage Axial-flow Research Compressor with Long- and Medium-chord Lengths in the Two Transonic Inlet Stages written by Gilbert K. Sievers and published by . This book was released on 1958 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: The chords of the first two stages of an eight-stage axial-flow compressor with two transonic inlet stages were doubled, and the effects of Reynolds number on the over-all performance were investigated and compared with those of the original compressor.
Author : Gregory Brenton Shirley
Publisher :
ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.:/5 (424 download)
Download or read book An Experimental Investigation of a Low Reynolds Number, High Mach Number Centrifugal Compressor written by Gregory Brenton Shirley and published by . This book was released on 1998 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Richard P. Geye
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (93 download)
Download or read book Investigation of Effects of Reynolds Number on Over-all Performance of an Eight-stage Axial-flow Research Compressor with Two Transonic Inlet Stages written by Richard P. Geye and published by . This book was released on 1957 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : David G. Schnorenberg
Publisher :
ISBN 13 : 9781423582878
Total Pages : 142 pages
Book Rating : 4.5/5 (828 download)
Download or read book Investigation of the Effect of Reynolds Number on Laminar Separation Bubbles on Controlled-Diffusion Compressor Blades in Cascade written by David G. Schnorenberg and published by . This book was released on 1996-06-01 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt: Detailed experimental investigation of second generation, controlled diffusion, compressor stator blades at an off-design inlet flow angle was performed in a low speed cascade wind tunnel using various experimental procedures. The objective of the study was the characterization of the off- design flow and the detailed investigation of flow separation which occurred near midchord. When it was found that the flow separation behavior was strongly influenced by the Reynolds number, the effect of Reynolds number variation on flow separation was investigated. Surface flow visualization was performed to gain general insight into the flow behavior. Blade surface pressure measurements were obtained using instrumented blades, from which coefficients of pressure were calculated. Laser Doppler velocimetry (LDV) was used to characterize the off-design flow upstream, in the passage between two blades, in the boundary layer on the suction side of the blades, and in the wake region. Overall, good comparisons between blade surface pressure measurements, LDV data and flow visualization were obtained for the separation region. At the highest Reynolds number, separation was turbulent and three dimensional and at the low Reynolds number the separation was predominately laminar and two dimensional.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 496 pages
Book Rating : 4.3/5 ( download)
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Carl Weigel
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)
Download or read book Reynolds Number Effect on Overall Performance of a 10.8-centimeter (4.25-IN.) Sweptback-bladed Centrifugal Compressor written by Carl Weigel and published by . This book was released on 1972 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Laurence J. Heidelberg
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (31 download)
Download or read book Effect of Reynolds Number on Overall Performance of a 3.7-inch-diameter Six-stage Axial-flow Compressor written by Laurence J. Heidelberg and published by . This book was released on 1972 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 692 pages
Book Rating : 4.3/5 (91 download)
Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1948 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Author :
Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.:/5 (319 download)
Download or read book National Bureau of Standards Circular written by and published by . This book was released on 1954 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 568 pages
Book Rating : 4.3/5 ( download)
Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Laurence J. Heidelberg
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.:/5 (249 download)
Download or read book Effect of Reynolds Number on Overall Performance of a 6-inch Radial Bladed Centrifugal Compressor written by Laurence J. Heidelberg and published by . This book was released on 1970 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: "Overall performance is presented over a range of compressor inlet pressures from a nominal 1.5 to 8.6 psia (l.0xl04 to 5.9x104 N/m2 abs) and corresponding Reynolds number range of 0.32X106 to 1.8X106. As inlet pressure and thus Reynolds number was decreased, a progressive degradation in efficiency along with a lowering of the surge and maximum flow points was observed. These changes in performance are explained in terms of changing viscous losses and changing effective flow areas with Reynolds number. A comparison between the data and the commonly used 0.2 power of Reynolds number relation to loss is made".--P. [i].
Author :
Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.3/5 (91 download)
Download or read book Circular of the Bureau of Standards written by and published by . This book was released on 1954 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : M. V. Casey
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)
Download or read book Effects of Reynolds Number on the Efficiency of Centrifugal Compressor Stages written by M. V. Casey and published by . This book was released on 1984 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 1256 pages
Book Rating : 4.F/5 ( download)
Download or read book Jet Propulsion written by and published by . This book was released on 1954 with total page 1256 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John D. Stanitz
Publisher :
ISBN 13 :
Total Pages : 712 pages
Book Rating : 4.F/5 ( download)
Download or read book Two-dimensional Compressible Flow in Centrifugal Compressors with Straight Blades written by John D. Stanitz and published by . This book was released on 1949 with total page 712 pages. Available in PDF, EPUB and Kindle. Book excerpt: Six numerical examples are presented for steady, two-dimensional, compressible, nonviscous flow in centrifugal compressors with straight blades. A seventh example is presented for incompressible flow. The solutions also applye to radial-flow turbines with rotation and flow direction reversed. The effects of variations in following parameters were investigated: (1) flow rate, (2) impeller-tip speed, (3) variation of passage height with radius, and (4) number of blades. The numerical results are presented in plots of the streamlines, constant Mach number lines, and constant pressure-ratio lines. Correlation equations are developed whereby the flow conditions in any impeller with straight blades can be determined for all operating conditions.
