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Book A Revised Computer Program for Axial Compressor Design  Volume 1  Theory  Descriptions  and User s Instructions

Download or read book A Revised Computer Program for Axial Compressor Design Volume 1 Theory Descriptions and User s Instructions written by Richard M. Hearsey and published by . This book was released on 1975 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report, in two volumes, describes a computer program that has been developed for the design of axial compressors. The principal purpose of the program is to enable a single computer program to determine the geometry of the compressor blading, details of the flow within the compressor, and the design point performance of the machine. Some optional calculation routines will also enable effects of mixing of the flow to be investigated. The program consists fundamentally of three sections; two alternative means of determining blade geometry, and an aerodynamic computation for the flow through the compressor.

Book A Revised Computer Program for Axial Compressor Design  Volume 1  Theory  Descriptions  and User s Instructions

Download or read book A Revised Computer Program for Axial Compressor Design Volume 1 Theory Descriptions and User s Instructions written by Richard M. Hearsey and published by . This book was released on 1975 with total page 117 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report, in two volumes, describes a computer program that has been developed for the design of axial compressors. The principal purpose of the program is to enable a single computer program to determine the geometry of the compressor blading, details of the flow within the compressor, and the design point performance of the machine. Some optional calculation routines will also enable effects of mixing of the flow to be investigated. The program consists fundamentally of three sections; two alternative means of determining blade geometry, and an aerodynamic computation for the flow through the compressor.

Book A Computer Program for Axial Compressor Design  Volume I  Theory Descriptions  and Users Instructions

Download or read book A Computer Program for Axial Compressor Design Volume I Theory Descriptions and Users Instructions written by Richard M. Hearsey and published by . This book was released on 1973 with total page 97 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computer program for the design of axial compressors is presented. It comprises of three principal sections; two alternative means of determining blade geometry, and an aerodynamic computation for the flow through the compressor. One method of determining blade geometry revolves around the use of various analytic meanlines for the blade sections, and leads to the aerodynamic analysis of the flow through specified blading. The other method consists of creating arbitrary blade sections to follow the flow directions previously determined in an aerodynamic design calculation. The aerodynamic design section incorporates a loss calculation routine that may be used to estimate the design point performance of the compressor. The report describes the computer program, and gives all information necessary to use it. (Modified author abstract).

Book A Revised Computer Program for Axial Compressor Design

Download or read book A Revised Computer Program for Axial Compressor Design written by Richard M. Hearsey and published by . This book was released on 1975 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report, in two volumes, describes a computer program that has been developed for the design of axial compressors. The principal purpose of the program is to enable a single computer program to determine the geometry of the compressor blading, details of the flow within the compressor, and the design point performance of the machine. Some optional calculation routines will also enable effects of mixing of the flow to be investigated. The program consists fundamentally of three sections; two alternative means of determining blade geometry, and an aerodynamic computation for the flow through the compressor.

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aerothermodynamics of Aircraft Engine Components

Download or read book Aerothermodynamics of Aircraft Engine Components written by Gordon C. Oates and published by AIAA. This book was released on 1985 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt: Annotation Design and R & D engineers and students will value the comprehensive, meticulous coverage in this volume. Beginning with the basic principles and concepts of aeropropulsion combustion, chapters explore specific processes, limitations, and analytical methods as they bear on component design.

Book The Aerothermodynamics of Aircraft Gas Turbine Engines

Download or read book The Aerothermodynamics of Aircraft Gas Turbine Engines written by and published by . This book was released on 1978 with total page 770 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book ASME Technical Papers

Download or read book ASME Technical Papers written by and published by . This book was released on with total page 492 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Computer Programs for Single stage Axial Compressor Test Data Analysis

Download or read book Computer Programs for Single stage Axial Compressor Test Data Analysis written by Richard M. Hearsey and published by . This book was released on 1973 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt: A pair of special-purpose computer programs have been written for the analysis of axial compressor aerodynamic test data. The axisymmetric flow of a thermal-perfect compressible fluid is assumed, and the streamline curvature method of solution is employed. By optionally incorporating details of the blade geometry in the input data, a detailed account of the flow through the blading may be obtained. A unique feature of the analysis is the option to determine annulus blockage due to boundary layers and blade wakes by utilizing experimental wall static pressure readings in addition to the usual traverses of total pressures and temperature. This first volume of two that describe the programs fully details the theory of the method, describes the computer programs, and gives all information necessary to use them.

Book NASA Conference Publication

Download or read book NASA Conference Publication written by and published by . This book was released on 1991 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 828 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aeronautical Engineering

Download or read book Aeronautical Engineering written by and published by . This book was released on 1993 with total page 712 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)

Book Computational Fluid Dynamics Symposium on Aeropropulsion

Download or read book Computational Fluid Dynamics Symposium on Aeropropulsion written by and published by . This book was released on 1991 with total page 696 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Revised Computer Program for Axial Compressor Design

Download or read book A Revised Computer Program for Axial Compressor Design written by Richard M. Hearsey and published by . This book was released on 1975 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: This report, in two volumes, describes a computer program that has been developed for the design of axial compressors. The principal purpose of the program is to enable a single computer program to determine the geometry of the compressor blading, details of the flow within the compressor, and the design point performance of the machine. Some optional calculation routines will also enable effects of mixing of the flow to be investigated. The program consists fundamentally of three sections; two alternative means of determining blade geometry, and an aerodynamic computation for the flow through the compressor.

Book A Revised Computer Program for Axial Compressor Design  Volume 2  Program Listing and Program Use Example

Download or read book A Revised Computer Program for Axial Compressor Design Volume 2 Program Listing and Program Use Example written by Richard M. Hearsey and published by . This book was released on 1975 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computer program for the design of axial compressors is presented. It comprises of three principal sections; two alternative means of determining blade geometry, and an aerodynamic computation for the flow through the compressor. The report shows the Fortran program listing and an example of the use of the program.

Book Government reports annual index

Download or read book Government reports annual index written by and published by . This book was released on 199? with total page 1216 pages. Available in PDF, EPUB and Kindle. Book excerpt: