Effects of Axial-plane Curvature and Passage-area Variation on Flow Capacity of Radial-discharge Impeller with Conventional Inlet Buckets

Download Effects of Axial-plane Curvature and Passage-area Variation on Flow Capacity of Radial-discharge Impeller with Conventional Inlet Buckets PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 560 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!


Book Synopsis Effects of Axial-plane Curvature and Passage-area Variation on Flow Capacity of Radial-discharge Impeller with Conventional Inlet Buckets by : William K. Ritter

Download or read book Effects of Axial-plane Curvature and Passage-area Variation on Flow Capacity of Radial-discharge Impeller with Conventional Inlet Buckets written by William K. Ritter and published by . This book was released on 1946 with total page 560 pages. Available in PDF, EPUB and Kindle. Book excerpt: It was concluded that the volume flow capacity of a conventional-type radial-discharge impeller may be greatly increased by utilizing a rear shroud profile of large radius of curvature and a large impeller axial depth to give a gradual change in direction tthrough the impeller passage.

Technical Note - National Advisory Committee for Aeronautics

Download Technical Note - National Advisory Committee for Aeronautics PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 280 pages
Book Rating : 4.:/5 (319 download)

DOWNLOAD NOW!


Book Synopsis Technical Note - National Advisory Committee for Aeronautics by :

Download or read book Technical Note - National Advisory Committee for Aeronautics written by and published by . This book was released on 1949 with total page 280 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Aerodynamic-thermodynamic Study of Centrifugal Compressors

Download An Aerodynamic-thermodynamic Study of Centrifugal Compressors PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis An Aerodynamic-thermodynamic Study of Centrifugal Compressors by : Gene Thomas Colwell

Download or read book An Aerodynamic-thermodynamic Study of Centrifugal Compressors written by Gene Thomas Colwell and published by . This book was released on 1962 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Note

Download Technical Note PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 486 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Technical Note by :

Download or read book Technical Note written by and published by . This book was released on 1949 with total page 486 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering Review

Download Aeronautical Engineering Review PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 596 pages
Book Rating : 4.:/5 (319 download)

DOWNLOAD NOW!


Book Synopsis Aeronautical Engineering Review by :

Download or read book Aeronautical Engineering Review written by and published by . This book was released on 1946 with total page 596 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Journal of the Royal Aeronautical Society

Download Journal of the Royal Aeronautical Society PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 634 pages
Book Rating : 4.:/5 (318 download)

DOWNLOAD NOW!


Book Synopsis Journal of the Royal Aeronautical Society by :

Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1947 with total page 634 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft

Download A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 492 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft by : Clifford J. Moore

Download or read book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft written by Clifford J. Moore and published by . This book was released on 1970 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report investigates critical reviews of NACA and NASA report literature on light aircraft design, with emphasis on propulsion subsystems, stability, control, propellers, performance, and safety.

NASA Contractor Report

Download NASA Contractor Report PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 1008 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis NASA Contractor Report by : United States. National Aeronautics and Space Administration

Download or read book NASA Contractor Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1970 with total page 1008 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Cumulative Title Index to United States Public Documents, 1789-1976

Download Cumulative Title Index to United States Public Documents, 1789-1976 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 560 pages
Book Rating : 4.:/5 (321 download)

DOWNLOAD NOW!


Book Synopsis Cumulative Title Index to United States Public Documents, 1789-1976 by : Daniel W. Lester

Download or read book Cumulative Title Index to United States Public Documents, 1789-1976 written by Daniel W. Lester and published by . This book was released on 1980 with total page 560 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft. Volume 3 - Propulsion Subsystems, Performance, Stability and Control, Propellers, and Flight Safety

Download A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft. Volume 3 - Propulsion Subsystems, Performance, Stability and Control, Propellers, and Flight Safety PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 492 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!


Book Synopsis A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft. Volume 3 - Propulsion Subsystems, Performance, Stability and Control, Propellers, and Flight Safety by : Clifford J. Moore

Download or read book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft. Volume 3 - Propulsion Subsystems, Performance, Stability and Control, Propellers, and Flight Safety written by Clifford J. Moore and published by . This book was released on 1970 with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Gas Turbine and Free Piston Engine Lectures, July 7-July 11, 1958

Download Gas Turbine and Free Piston Engine Lectures, July 7-July 11, 1958 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 698 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis Gas Turbine and Free Piston Engine Lectures, July 7-July 11, 1958 by : Frank L Schwartz

Download or read book Gas Turbine and Free Piston Engine Lectures, July 7-July 11, 1958 written by Frank L Schwartz and published by . This book was released on 1958 with total page 698 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Gas Turbine Lectures, June 29-July 10, 1953

Download Gas Turbine Lectures, June 29-July 10, 1953 PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 742 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis Gas Turbine Lectures, June 29-July 10, 1953 by : University of Michigan. College of Engineering. Dept. of Mechanical and Industrial Engineering

Download or read book Gas Turbine Lectures, June 29-July 10, 1953 written by University of Michigan. College of Engineering. Dept. of Mechanical and Industrial Engineering and published by . This book was released on 1953 with total page 742 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Gas Turbine and Free Piston Engine Lectures, June 13-June 17, 1955, Department of Mechanical and Industrial Engineering, University of Michigan

Download Gas Turbine and Free Piston Engine Lectures, June 13-June 17, 1955, Department of Mechanical and Industrial Engineering, University of Michigan PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 676 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!


Book Synopsis Gas Turbine and Free Piston Engine Lectures, June 13-June 17, 1955, Department of Mechanical and Industrial Engineering, University of Michigan by : Frank L. Schwartz

Download or read book Gas Turbine and Free Piston Engine Lectures, June 13-June 17, 1955, Department of Mechanical and Industrial Engineering, University of Michigan written by Frank L. Schwartz and published by . This book was released on 1955 with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt:

United States Government Publications Monthly Catalog

Download United States Government Publications Monthly Catalog PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.3/5 (121 download)

DOWNLOAD NOW!


Book Synopsis United States Government Publications Monthly Catalog by :

Download or read book United States Government Publications Monthly Catalog written by and published by . This book was released on 1948 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Visual Observations of Flow Through a Radial-bladed Centrifugal Impeller

Download Visual Observations of Flow Through a Radial-bladed Centrifugal Impeller PDF Online Free

Author :
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

DOWNLOAD NOW!


Book Synopsis Visual Observations of Flow Through a Radial-bladed Centrifugal Impeller by : Richard F. Soltis

Download or read book Visual Observations of Flow Through a Radial-bladed Centrifugal Impeller written by Richard F. Soltis and published by . This book was released on 1968 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Radial Flow Turbocompressors

Download Radial Flow Turbocompressors PDF Online Free

Author :
Publisher : Cambridge University Press
ISBN 13 : 1108416675
Total Pages : 789 pages
Book Rating : 4.1/5 (84 download)

DOWNLOAD NOW!


Book Synopsis Radial Flow Turbocompressors by : Michael Casey

Download or read book Radial Flow Turbocompressors written by Michael Casey and published by Cambridge University Press. This book was released on 2021-06-10 with total page 789 pages. Available in PDF, EPUB and Kindle. Book excerpt: An introduction to the theory and engineering practice that underpins the component design and analysis of radial flow turbocompressors. Drawing upon an extensive theoretical background and years of practical experience, the authors provide descriptions of applications, concepts, component design, analysis tools, performance maps, flow stability, and structural integrity, with illustrative examples. Features wide coverage of all types of radial compressor over many applications unified by the consistent use of dimensional analysis. Discusses the methods needed to analyse the performance, flow, and mechanical integrity that underpin the design of efficient centrifugal compressors with good flow range and stability. Includes explanation of the design of all radial compressor components, including inlet guide vanes, impellers, diffusers, volutes, return channels, de-swirl vanes and side-streams. Suitable as a reference for advanced students of turbomachinery, and a perfect tool for practising mechanical and aerospace engineers already within the field and those just entering it.

Effects of Impeller-Diffuser Interaction on Centrifugal Compressor Performance

Download Effects of Impeller-Diffuser Interaction on Centrifugal Compressor Performance PDF Online Free

Author :
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781720484141
Total Pages : 68 pages
Book Rating : 4.4/5 (841 download)

DOWNLOAD NOW!


Book Synopsis Effects of Impeller-Diffuser Interaction on Centrifugal Compressor Performance by : National Aeronautics and Space Administration (NASA)

Download or read book Effects of Impeller-Diffuser Interaction on Centrifugal Compressor Performance written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-30 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: This research program focuses on characterizing the effect of impeller-diffuser interactions in a centrifugal compressor stage on its performance using unsteady threedimensional Reynolds-averaged Navier-Stokes simulations. The computed results show that the interaction between the downstream diffuser pressure field and the impeller tip clearance flow can account for performance changes in the impeller. The magnitude of performance change due to this interaction was examined for an impeller with varying tip clearance followed by a vaned or vaneless diffuser. The impact of unsteady impeller-diffuser interaction, primarily through the impeller tip clearance flow, is reflected through a time-averaged change in impeller loss, blockage and slip. The results show that there exists a tip clearance where the beneficial effect of the impeller-diffuser interaction on the impeller performance is at a maximum. A flow feature that consists of tip flow back leakage was shown to occur at design speed for the centrifugal compressor stage. This flow phenomenon is described as tip flow that originates in one passage, flows downstream of the impeller trailing edge and then returns to upstream of the impeller trailing edge of a neighboring passage. Such a flow feature is a source of loss in the impeller. A hypothesis is put forth to show that changing the diffuser vane count and changing impeller-diffuser gap has an analogous effect on the impeller performance. The centrifugal compressor stage was analyzed using diffusers of different vane counts, producing an impeller performance trend similar to that when the impeller-diffuser gap was varied, thus supporting the hypothesis made. This has the implication that the effect impeller performance associated with changing the impeller-diffuser gap and changing diffuser vane count can be described by the non-dimensional ratio of impeller-diffuser gap to diffuser vane pitch. A procedure is proposed and developed for isolating impeller passage b