Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Advancement Of Small Gas Turbine Component Technology Advanced Small Axial Compressor Volume I Analysis And Design
Download Advancement Of Small Gas Turbine Component Technology Advanced Small Axial Compressor Volume I Analysis And Design full books in PDF, epub, and Kindle. Read online Advancement Of Small Gas Turbine Component Technology Advanced Small Axial Compressor Volume I Analysis And Design ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Advancement of Small Gas Turbine Component Technology, Advanced Small Axial Compressor. Volume I. Analysis and Design by : James V. Davis
Download or read book Advancement of Small Gas Turbine Component Technology, Advanced Small Axial Compressor. Volume I. Analysis and Design written by James V. Davis and published by . This book was released on 1969 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt: A cursory design study of the gas generator involving the preliminary design and analysis of a family of axial compressors was conducted. Each axial compressor was designed to be capable of match with advanced centrifugal technology. The minimum overall axial-centrifugal design pressure ratio for each compressor configuration was 16:1. The engine performance using the characteristics of the compressor designs was evaluated and an optimum gas generator configuration was selected. The axial compressor for the optimum gas generator configuration was detail designed for test rig evaluation. This axial compressor has two stages and a 3.0:1 design pressure ratio. The design flow rate is 5.0 pound-per-second and the inlet tip radius is 2.72 inches. (Author).
Book Synopsis Advancement of Small Gas Turbine Component Technology, Advanced Small Axial Compressor. Volume I. Analysis and Design. Addendum by : James V. Davis
Download or read book Advancement of Small Gas Turbine Component Technology, Advanced Small Axial Compressor. Volume I. Analysis and Design. Addendum written by James V. Davis and published by . This book was released on 1969 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: A complete two-stage aerodynamic axial compressor design capable of being matched with the USAAVLABS advanced centrifugal technology was prepared. Fully variable part span inlet guide vanes were designed. Two transition ducts were also designed to provide an efficient aerodynamic flow path from the axial compressor exit to the centrifugal compressor inlet. (Author).
Book Synopsis Advancement of Small Gas Turbine Component Technology by : James V. Davis
Download or read book Advancement of Small Gas Turbine Component Technology written by James V. Davis and published by . This book was released on 1970* with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents the redesign analysis of a two-stage axial compressor program for the advancement of small gas turbine component technology. The discussion covers fabrication, test, and redesign of the axial compressor which was presented in Volume I. (Author).
Book Synopsis Advancement of Small Gas Turbine Component Technology Advanced Small Axial Compressor. Volume II. Test and Redesign by : James V. Davis
Download or read book Advancement of Small Gas Turbine Component Technology Advanced Small Axial Compressor. Volume II. Test and Redesign written by James V. Davis and published by . This book was released on 1970 with total page 173 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents the redesign analysis of a two-stage axial compressor program for the advancement of small gas turbine component technology. The discussion covers fabrication, test, and redesign of the axial compressor which was presented in Volume I. (Author).
Book Synopsis Advancement of Small Gas Turbine Component Technology, Advanced Small Axial Compressor. Volume II. Addendum. Aerodynamic Redesign by : James V. Davis
Download or read book Advancement of Small Gas Turbine Component Technology, Advanced Small Axial Compressor. Volume II. Addendum. Aerodynamic Redesign written by James V. Davis and published by . This book was released on 1970 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the redesign analysis of the axial compressor program for the advancement of small gas turbine component technology. A two-stage axial compressor was redesigned using test data from the previous two stage tests together with an analysis of a family of high-pressure-ratio compressor rotors. The major changes made to the original design were reduced solidity in both rotors, increased first-stage rotor aspect ratio, and modified first-stage rotor blade profile.
Book Synopsis Small Gas Turbine Engine Component Technology - Turbine. Volume I. Phase i Summary Report by : T. Schober
Download or read book Small Gas Turbine Engine Component Technology - Turbine. Volume I. Phase i Summary Report written by T. Schober and published by . This book was released on 1968 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes the aerodynamic, thermal, and mechanical design and analysis, fabrication, and experimental evaluation of a transpiration cooled, single stage axial-flow turbine component capable of operation at 2500F average inlet temperature. Combustor design and development and test rig design are described, as well as stator vane hot thermal and cold aerodynamic cascade testing. The objective of the program was to advance and demonstrate high turbine inlet technology for use in a gas generator with a compressor pressure ratio of 8 to 10 and an airflow of 4 pounds per second. Additional objectives included turbine work of 140 Btu per pound of airflow at a high level of turbine efficienty. Phase I report presents the design and analysis. It was concluded that the advanced technology incorporated in the turbine design relative to blade cooling and turbine mechanical integrity are practical and can be applied to the design of advanced small gas turbines. (Author).
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 818 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Single-Stage Axial Compressor Component Development for Small Gas Turbine Engines. Volume I. Design by : Charles H. Muller
Download or read book Single-Stage Axial Compressor Component Development for Small Gas Turbine Engines. Volume I. Design written by Charles H. Muller and published by . This book was released on 1969 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt: The design of a single stage axial supersonic compressor with a predicted performance of 2.8:1 stage pressure ratio at 82% adiabatic efficiency and 4 lb/sec airflow is discussed. The results of a gas generator performance study to evaluate non-regenerated designs with 16:1 pressure ratio compressors and turbine inlet temperatures between 2500 F and 3000 F are presented and discussed. The design point specific fuel consumption of the engines studied ranged from 0.415 to 0.438 lb/hp/hr. At 50% power this range increased to 0.465 and 0.534 respectively. The engine configuration which indicated the lowest specific fuel consumption has a two spool gas generator and variable stator free power turbine. The preliminary designs of a two stage axial/centrifugal compressor and an advanced gas generator which incorporates this compressor are discussed. The predicted performance of the compressor is 16:1 pressure ratio at an adiabatic efficiency of 77.5% and an airflow of 4 lb/sec. The predicted design point specific fuel consumption and power at a 2500 F turbine inlet temperature are 0.431 lb/hp/hr and 785 hp respectively. The results of a preliminary design study for a variable geometry axial compressor rotor concept are also discussed. This concept offers the potential for improved part speed compressor performance and stage matching. (Author).
Book Synopsis Single-Stage Axial Compressor Component Development for Small Gas Turbine Engines. Volume II. Rotor Development by : Charles H. Muller
Download or read book Single-Stage Axial Compressor Component Development for Small Gas Turbine Engines. Volume II. Rotor Development written by Charles H. Muller and published by . This book was released on 1969 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes the development of the rotor for the 2.8:1 single stage supersonic axial compressor design. The rotor performance was evaluated through experimental testing with the inlet guide vanes but without the exit stator. The experimental results are analyzed and compared to the design data and criteria. Although a circumferential flow distortion at the rotor exit prevented a very accurate assessment of the performance potential, the data provided ample evidence that the rotor performance goals could be met with uniform exit conditions. The presence of the exit stator during the stage development tests in the subsequent phase was expected to reduce the flow distortion at the rotor exit to near uniform conditions. (Author).
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. Congress. Senate. Committee on Appropriations. Subcommittee on Department of Defense Publisher : ISBN 13 : Total Pages :1088 pages Book Rating :4.3/5 (121 download)
Book Synopsis Department of the Army by : United States. Congress. Senate. Committee on Appropriations. Subcommittee on Department of Defense
Download or read book Department of the Army written by United States. Congress. Senate. Committee on Appropriations. Subcommittee on Department of Defense and published by . This book was released on 1970 with total page 1088 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. Congress. Senate. Committee on Appropriations. Subcommittee on Department of Defense Publisher : ISBN 13 : Total Pages :2284 pages Book Rating :4.:/5 (319 download)
Book Synopsis Department of Defense Appropriations for Fiscal Year 1971 by : United States. Congress. Senate. Committee on Appropriations. Subcommittee on Department of Defense
Download or read book Department of Defense Appropriations for Fiscal Year 1971 written by United States. Congress. Senate. Committee on Appropriations. Subcommittee on Department of Defense and published by . This book was released on 1970 with total page 2284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Department of Defense Appropriations for Fiscal Year 1971: Dept. of Defense, defense agencies, public witnesses by : United States. Congress. Senate. Appropriations Committee
Download or read book Department of Defense Appropriations for Fiscal Year 1971: Dept. of Defense, defense agencies, public witnesses written by United States. Congress. Senate. Appropriations Committee and published by . This book was released on 1970 with total page 1178 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Gas Turbine Design, Components and System Design Integration by : Meinhard T. Schobeiri
Download or read book Gas Turbine Design, Components and System Design Integration written by Meinhard T. Schobeiri and published by Springer. This book was released on 2017-06-06 with total page 522 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book written by a world-renowned expert with more than forty years of active gas turbine R&D experience comprehensively treats the design of gas turbine components and their integration into a complete system. Unlike many currently available gas turbine handbooks that provide the reader with an overview without in-depth treatment of the subject, the current book is concentrated on a detailed aero-thermodynamics, design and off-deign performance aspects of individual components as well as the system integration and its dynamic operation.This new book provides practicing gas turbine designers and young engineers working in the industry with design material that the manufacturers would keep proprietary. The book is also intended to provide instructors of turbomachinery courses around the world with a powerful tool to assign gas turbine components as project and individual modules that are integrated into a complete system. Quoting many statements by the gas turbine industry professionals, the young engineers graduated from the turbomachinery courses offered by the author, had the competency of engineers equivalent to three to four years of industrial experience.
Book Synopsis Research and Technology Objectives and Plans Summary by :
Download or read book Research and Technology Objectives and Plans Summary written by and published by . This book was released on with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt: "A compilation of the summary portions of each of the RTOPs used for management review and control of research currently in progress throughout NASA"--P. i.
Author :United States. Congress. Senate. Select Committee on Small Business Publisher : ISBN 13 : Total Pages :572 pages Book Rating :4.:/5 (327 download)
Book Synopsis Technology and Management Assistance Programs of the Small Business Administration by : United States. Congress. Senate. Select Committee on Small Business
Download or read book Technology and Management Assistance Programs of the Small Business Administration written by United States. Congress. Senate. Select Committee on Small Business and published by . This book was released on 1976 with total page 572 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Energy Research Abstracts written by and published by . This book was released on 1981 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt:
