Download or read book Aerodynamic Design Performance Predictions of a Single Stage Axial flow Turbine written by Angel Santos and published by . This book was released on 1993 with total page 288 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Turbine Aerodynamics written by Ronald H. Aungier and published by American Society of Mechanical Engineers. This book was released on 2006 with total page 424 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book provides a thorough description of actual, working aerodynamic design and analysis systems, for both axial-flow and radial-flow turbines. It describes the basic fluid dynamic and thermodynamic principles, empirical models and numerical methods used for the full range of procedures and analytical tools that an engineer needs for virtually any type of aerodynamic design or analysis activity for both types of turbine. The book includes sufficient detail for readers to implement all or part of the systems. The author provides practical and effective design strategies for applying both turbine types, which are illustrated by design examples. Comparisons with experimental results are included to demonstrate the prediction accuracy to be expected. This book is intended for practicing engineers concerned with the design and development of turbines and related machinery.
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:
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:
Download or read book Off design Performance Prediction with Experimental Verification for a Radial inflow Turbine written by Samuel M. Futral and published by . This book was released on 1965 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Analysis of Single Stage Axial flow Turbine Performance Using Three dimensional Calculating Methods written by Robert Glen Harrison and published by . This book was released on 1967 with total page 145 pages. Available in PDF, EPUB and Kindle. Book excerpt: The method of turbine performance prediction developed by Vavra and Eckert has been refined in this analysis to realize more of the potential of the three-dimensional calculating methods. Mach number and rotor tip clearance effects on blade outlet angles and loss coefficients have been localized rather than averaged over the blade height. An approximation for streamline curvature has been used. Performance curves were determined for two single stage axial-flow turbines. Test results were available for one of the turbines. Agreement between predicted and experimental performance values was generally within 3 per cent. (Author).
Download or read book Axial Turbine Aerodynamics for Aero engines written by Zhengping Zou and published by Springer. This book was released on 2018-01-11 with total page 572 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is a monograph on aerodynamics of aero-engine gas turbines focusing on the new progresses on flow mechanism and design methods in the recent 20 years. Starting with basic principles in aerodynamics and thermodynamics, this book systematically expounds the recent research on mechanisms of flows in axial gas turbines, including high pressure and low pressure turbines, inter-turbine ducts and turbine rear frame ducts, and introduces the classical and innovative numerical evaluation methods in different dimensions. This book also summarizes the latest research achievements in the field of gas turbine aerodynamic design and flow control, and the multidisciplinary conjugate problems involved with gas turbines. This book should be helpful for scientific and technical staffs, college teachers, graduate students, and senior college students, who are involved in research and design of gas turbines.
- Author : Milton G. Kofskey
- Publisher :
- Release : 1968
- ISBN :
- Pages : 36 pages
Aerodynamic Evaluation of Two stage Axial flow Turbine Designed for Brayton cycle Space Power System
Download or read book Aerodynamic Evaluation of Two stage Axial flow Turbine Designed for Brayton cycle Space Power System written by Milton G. Kofskey and published by . This book was released on 1968 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Cold air Performance of a 12 766 centimeter tip diameter Axial flow Cooled Turbine written by Jeffrey E. Haas and published by . This book was released on 1975 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: A solid blade version of a single-stage, axial-flow turbine was investigated to determine its performance over a range of speeds from 0 to 105 percent of equivalent design speed and over a range of total to static pressure ratios from 1.62 to 5.07.
Download or read book An Analysis of Single Stage Axial flow Turbine Performance Using Three dimensional Calculating Methods written by and published by . This book was released on 1967 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The method of turbine performance prediction developed by Vavra and Eckert has been refined in this analysis to realize more of the potential of the three-dimensional calculating methods. Mach number and rotor tip clearance effects on blade outlet angles and loss coefficients have been localized rather than averaged over the blade height. An approximation for streamline curvature has been used. Performance curves were determined for two single stage axial-flow turbines. Test results were available for one of the turbines. Agreement between predicted and experimental performance values was generally within 3 per cent. (Author).
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1982 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance in Air of 4 inch 10 16 cm Mean diameter Single stage Axial flow Turbine for Reynolds Numbers from 4900 to 188 000 written by Hugh A. Klassen and published by . This book was released on 1968 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by United States. National Aeronautics and Space Administration and published by . This book was released on 1977 with total page 964 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Design and Experimental Investigation of a High weight flow Low pressure ratio Turbine written by Donald A. Petrash and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Performance Prediction of a Multi stage Axial Flow Turbine written by Jonathan B. Roberts and published by . This book was released on 1988 with total page 290 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Axial Turbine Loss Analysis and Efficiency Prediction Method written by Yong S. Hong and published by . This book was released on 1966 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented to predict axial stage turbine efficiency using detailed aerodynamic component losses. Suitable computer programs were set up for the more time consuming portions of the calculations. Boundary layer theory plus empirical test data was used to obtain numerical values for the flow losses. The method was applied to typical Boeing turbine tests and stage efficiencies were compared with the measured values. Calculated and measured stage efficiencies agreed within plus or minus one percent in all cases. This achievement proved to be far superior to existing prediction methods which yielded efficiency accuracies ranging from 2 to 7 percent. Using the developed method, the performance of a given turbine stage can be optimized without spending an excessive amount of time for numerical calculations by evaluating various combination of aspect ratio, solidity, number of blades, trailing edge thickness, and rotor tip clearance. All the investigated cases were checked for only single stage axial turbines. The accuracy of the method for multi-stage application has yet to be verified by experiment. (Author).