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Loss Distributions In Axial Flow Compressor Blade Rows
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Book Synopsis Loss Distributions in Axial-flow Compressor Blade Rows by :
Download or read book Loss Distributions in Axial-flow Compressor Blade Rows written by and published by . This book was released on 1981 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Method for Predicting Off-design Performance of Axial-flow Compressor Blade Rows by : George K. Serovy
Download or read book Method for Predicting Off-design Performance of Axial-flow Compressor Blade Rows written by George K. Serovy and published by . This book was released on 1959 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Design of Axial Flow Compressors by : Robert O. Bullock
Download or read book Aerodynamic Design of Axial Flow Compressors written by Robert O. Bullock and published by . This book was released on 1965 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Design of Axial-flow Compressors by : Lewis Research Center
Download or read book Aerodynamic Design of Axial-flow Compressors written by Lewis Research Center and published by . This book was released on 1965 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
Book Synopsis Investigation of Blade-row Flow Distributions in Axial-flow-compressor Stage Consisting of Guide Vanes and Rotor-blade Row by : John J. Mahoney
Download or read book Investigation of Blade-row Flow Distributions in Axial-flow-compressor Stage Consisting of Guide Vanes and Rotor-blade Row written by John J. Mahoney and published by . This book was released on 1950 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Blade-row Flow Distributions in Axial-flow-compressor Stage Consisting of Guide and Rotor-blade Row by : John J. Mahoney
Download or read book Investigation of Blade-row Flow Distributions in Axial-flow-compressor Stage Consisting of Guide and Rotor-blade Row written by John J. Mahoney and published by . This book was released on 1950 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental and Theoretical Distribution of Flow Produced by Inlet Guide Vanes of an Axial-flow Compressor by : Harold B. Finger
Download or read book Experimental and Theoretical Distribution of Flow Produced by Inlet Guide Vanes of an Axial-flow Compressor written by Harold B. Finger and published by . This book was released on 1949 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented by which the velocities out of any blade row can be accurately computed from the energy, continuity, and simplified-radial-equilibrium equations if the flow angle if the flow angle and total enthalpy distributions are known.
Book Synopsis Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss by : Kenneth Lee Suder
Download or read book Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss written by Kenneth Lee Suder and published by . This book was released on 1996 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Method of Experimentally Determining Radial Distributions of Velocity Through Axial-flow Compressor by : Harold B. Finger
Download or read book Method of Experimentally Determining Radial Distributions of Velocity Through Axial-flow Compressor written by Harold B. Finger and published by . This book was released on 1950 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for determining the velocity distributions downstream of any compressor blade row if the outlet total temperatures, total pressures, and relative flow angles are known. The method has been applied to the determination of the velocities and the pressures in a 10-stage compressor and has indicated good agreement with the measured wall-static pressures.
Book Synopsis Experimental Investigation of a Transonic Compressor Cascade and Test Results for Four Blade Sections by : James C. Emery
Download or read book Experimental Investigation of a Transonic Compressor Cascade and Test Results for Four Blade Sections written by James C. Emery and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NACA Research Memorandum written by and published by . This book was released on 1958 with total page 488 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Tech Brief written by and published by . This book was released on 1968 with total page 634 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration Technology Utilization Division Publisher : ISBN 13 : Total Pages :574 pages Book Rating :4.F/5 ( download)
Book Synopsis NASA Tech Brief by : United States. National Aeronautics and Space Administration Technology Utilization Division
Download or read book NASA Tech Brief written by United States. National Aeronautics and Space Administration Technology Utilization Division and published by . This book was released on with total page 574 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Approximate design method for high-solidity blade elements in compressors and turbines by : John Stanitz
Download or read book Approximate design method for high-solidity blade elements in compressors and turbines written by John Stanitz and published by Рипол Классик. This book was released on 1951 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate blade-element design method is developed for compressible or incompressible nonviscous flow in high-solidity stators or rotors of axial-, radial-, or mixed-flow compressors, turbines, or two-dimensinal cascades. The method is based upon channel-type flow between blade elements on a specified surface of revolution that lies between the hub and shroud (casing) and is concentric with the axis of the compressor turbine. The blade elements is designed for prescribed velocities along the blade-element profile as a function of distance along meridonal lines on the surface of revolution. Two numerical examples are presented: (1) the design of a blade-element profile for a plane two-dimensional cascade in compressible flow with the prescribed velocities along the profiles; and (2) the design of a blade element for the impeller of a mixed-flow centrifugal compressor.
Download or read book NASA Technical Paper written by and published by . This book was released on 1983 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt: