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Book Computer Program for Preliminary Design Analysis of Axial flow Turbines

Download or read book Computer Program for Preliminary Design Analysis of Axial flow Turbines written by Arthur J. Glassman and published by . This book was released on 1972 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: The program method is based on a mean-diameter flow analysis. Input design requirements include power or pressure ratio, flow, temperature, pressure, and speed. Turbine designs are generated for any specified number of stages and for any of three types of velocity diagrams (symmetrical, zero exit swirl, or impulse). Exit turning vanes can be included in the design. Program output includes inlet and exit annulus dimensions, exit temperature and pressure, total and static efficiencies, blading angles, and last-stage critical velocity ratios. The report presents the analysis method, a description of input and output with sample cases, and the program listing.

Book Computer Program for Preliminary Design Analysis of Axial flow Turbines

Download or read book Computer Program for Preliminary Design Analysis of Axial flow Turbines written by Arthur J. Glassman and published by . This book was released on 1972 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Computer Code for Preliminary Sizing Analysis of Axial Flow Turbines

Download or read book Computer Code for Preliminary Sizing Analysis of Axial Flow Turbines written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-16 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: This mean diameter flow analysis uses a stage average velocity diagram as the basis for the computational efficiency. Input design requirements include power or pressure ratio, flow rate, temperature, pressure, and rotative speed. Turbine designs are generated for any specified number of stages and for any of three types of velocity diagrams (symmetrical, zero exit swirl, or impulse) or for any specified stage swirl split. Exit turning vanes can be included in the design. The program output includes inlet and exit annulus dimensions, exit temperature and pressure, total and static efficiencies, flow angles, and last stage absolute and relative Mach numbers. An analysis is presented along with a description of the computer program input and output with sample cases. The analysis and code presented herein are modifications of those described in NASA-TN-D-6702. These modifications improve modeling rigor and extend code applicability. Glassman, Arthur J. Unspecified Center NASA-CR-4430, E-6150, NAS 1.26:4430 NAG3-1165; RTOP 505-69-50...

Book Computer Code for Preliminary Sizing Analysis of Axial flow Turbines

Download or read book Computer Code for Preliminary Sizing Analysis of Axial flow Turbines written by Arthur J. Glassman and published by . This book was released on 1992 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Analysis of Geometry and Design Point Performance of Axial Flow Turbines  II   Computer Program

Download or read book Analysis of Geometry and Design Point Performance of Axial Flow Turbines II Computer Program written by A. F. Carter and published by . This book was released on 1968 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Originally issued as Northern Research and Engineering Report.

Book Analysis of Geometry and Design Point Performance of Axial Flow Turbines

Download or read book Analysis of Geometry and Design Point Performance of Axial Flow Turbines written by Northern Research and Engineering Corporation (Cambridge, Mass.) and published by . This book was released on 1968 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Computer Program Abstracts

Download or read book Computer Program Abstracts written by and published by . This book was released on 1975 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Tech Brief

Download or read book NASA Tech Brief written by and published by . This book was released on 1970 with total page 792 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Cumulative Index to NASA Tech Briefs

Download or read book Cumulative Index to NASA Tech Briefs written by United States. National Aeronautics and Space Administration and published by . This book was released on 1970 with total page 788 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalog of United States Government Publications  Cumulative Index

Download or read book Monthly Catalog of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1976 with total page 1408 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 1987 with total page 1126 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Book Fundamentals of Jet Propulsion with Applications

Download or read book Fundamentals of Jet Propulsion with Applications written by Ronald D. Flack and published by Cambridge University Press. This book was released on 2005-04-25 with total page 696 pages. Available in PDF, EPUB and Kindle. Book excerpt: This introductory 2005 text on air-breathing jet propulsion focuses on the basic operating principles of jet engines and gas turbines. Previous coursework in fluid mechanics and thermodynamics is elucidated and applied to help the student understand and predict the characteristics of engine components and various types of engines and power gas turbines. Numerous examples help the reader appreciate the methods and differing, representative physical parameters. A capstone chapter integrates the text material into a portion of the book devoted to system matching and analysis so that engine performance can be predicted for both on- and off-design conditions. The book is designed for advanced undergraduate and first-year graduate students in aerospace and mechanical engineering. A basic understanding of fluid dynamics and thermodynamics is presumed. Although aircraft propulsion is the focus, the material can also be used to study ground- and marine-based gas turbines and turbomachinery and some advanced topics in compressors and turbines.

Book Analysis of Geometry and Design Point Performance of Axial Flow Turbines

Download or read book Analysis of Geometry and Design Point Performance of Axial Flow Turbines written by M. Platt and published by . This book was released on 1968 with total page 332 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book COSMIC Software Catalog

Download or read book COSMIC Software Catalog written by and published by . This book was released on 1987 with total page 444 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Preliminary Axial Flow Turbine Design and Off Design Performance Analysis Methods for Rotary Wing Aircraft Engines

Download or read book Preliminary Axial Flow Turbine Design and Off Design Performance Analysis Methods for Rotary Wing Aircraft Engines written by Nasa Technical Reports Server (Ntrs) and published by BiblioGov. This book was released on 2013-07-01 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The NASA Technical Reports Server (NTRS) houses half a million publications that are a valuable means of information to researchers, teachers, students, and the general public. These documents are all aerospace related with much scientific and technical information created or funded by NASA. Some types of documents include conference papers, research reports, meeting papers, journal articles and more. This is one of those documents.