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Cold Air Investigation Of Effects Of Partial Admission On Performance Of 375 Inch Mean Diameter Single Stage Axial Flow Turbine
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Book Synopsis Cold-air Investigation of Effects of Partial Admission on Performance of 3.75-inch Mean-diameter Single-stage Axial-flow Turbine by : Hugh A. Klassen
Download or read book Cold-air Investigation of Effects of Partial Admission on Performance of 3.75-inch Mean-diameter Single-stage Axial-flow Turbine written by Hugh A. Klassen and published by . This book was released on 1968 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781726001458 Total Pages :38 pages Book Rating :4.0/5 (14 download)
Book Synopsis Cold Air Performance of a 12.766-Centimeter-Tip-Diameter Axial-Flow Cooled Turbine. 2 by : National Aeronautics and Space Administration (NASA)
Download or read book Cold Air Performance of a 12.766-Centimeter-Tip-Diameter Axial-Flow Cooled Turbine. 2 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-22 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: An air cooled version of a single-stage, axial-flow turbine was investigated to determine aerodynamic performance with and without air ejection from the stator and rotor blades surfaces to simulate the effect of cooling air discharge. Air ejection rate was varied from 0 to 10 percent of turbine mass flow for both the stator and the rotor. A primary-to-air ejection temperature ratio of about 1 was maintained. Haas, J. E. and Kofskey, M. G. Glenn Research Center NASA-TP-1018 RTOP 505-04...
Book Synopsis Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine by : Jeffrey E. Haas
Download or read book Cold-air performance of a 12.766-centimeter-tip axial-flow cooled turbine written by Jeffrey E. Haas and published by . This book was released on 1977 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air investigation of 3 1/2-stage fan-drive turbine with a stage loading factor of 4 designed for an integral lift engine by : Warren J. Whitney
Download or read book Cold-air investigation of 3 1/2-stage fan-drive turbine with a stage loading factor of 4 designed for an integral lift engine written by Warren J. Whitney and published by . This book was released on 1977 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air Performance of a 12.766-centimeter-tip-diameter Axial-flow Cooled Turbine. 3: Effect of Rotor Tip Clearance on Overall Performance of a Solid Blade Configuration by : Jeffrey E. Haas
Download or read book Cold-air Performance of a 12.766-centimeter-tip-diameter Axial-flow Cooled Turbine. 3: Effect of Rotor Tip Clearance on Overall Performance of a Solid Blade Configuration written by Jeffrey E. Haas and published by . This book was released on 1977 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two tip clearance configurations, one with a recess in the casing and the other with a reduced rotor blade height, were investigated at design equivalent speed over a range of tip clearance from about 2.0 to 5.0 percent of the stator blade height. The optimum configuration with a recess in the casing was the one where the rotor tip diameter was equal to the stator tip diameter (zero blade extension). For this configuration there was an approximate 1.5 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height. For the reduced blade height configurations there was an approximate 2.0 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height.
Book Synopsis Cold-air Investigation of a Turbine for High-temperature-engine Application: Two-stage turbine performance as affected by variable stator area by :
Download or read book Cold-air Investigation of a Turbine for High-temperature-engine Application: Two-stage turbine performance as affected by variable stator area written by and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Partial- and Full-admission Characteristics of a Two-stage Velocity-compounded Turbine by : Thomas P. Moffitt
Download or read book Experimental Investigation of Partial- and Full-admission Characteristics of a Two-stage Velocity-compounded Turbine written by Thomas P. Moffitt and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air investigation of 4 1/2-stage turbine with stage loading factor of 4.66 and high specific work output by :
Download or read book Cold-air investigation of 4 1/2-stage turbine with stage loading factor of 4.66 and high specific work output written by and published by . This book was released on 1977 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air Investigation of 4 1/2-stage Turbine with Stage-loading Factor of 4.66 and High Specific Work Output by : Warren J. Whitney
Download or read book Cold-air Investigation of 4 1/2-stage Turbine with Stage-loading Factor of 4.66 and High Specific Work Output written by Warren J. Whitney and published by . This book was released on 1980 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold Air Performance of a 12.766-centimeter-tip-diameter Axial-flow Cooled Turbine. 2: Effect of Air Ejection on Turbine Performance by :
Download or read book Cold Air Performance of a 12.766-centimeter-tip-diameter Axial-flow Cooled Turbine. 2: Effect of Air Ejection on Turbine Performance written by and published by . This book was released on 1977 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air Experimental Investigation of a Turbine with Blade Trailing Edge Coolant Ejection. 1 by : H. J. Schum
Download or read book Cold-air Experimental Investigation of a Turbine with Blade Trailing Edge Coolant Ejection. 1 written by H. J. Schum and published by . This book was released on 1975 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air Investigation of 4 1/2-stage Turbine with Stage-loading Factor of 4.66 and High Specific Work Output by :
Download or read book Cold-air Investigation of 4 1/2-stage Turbine with Stage-loading Factor of 4.66 and High Specific Work Output written by and published by . This book was released on 1980 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air Performance of a 12.766-centimeter-tip-diameter Axial-flow Cooled Turbine by : Jeffrey E. Haas
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 1977 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air Investigation of a Turbine for High-temperature-engine Application: Two-stage turbine performance by :
Download or read book Cold-air Investigation of a Turbine for High-temperature-engine Application: Two-stage turbine performance written by and published by . This book was released on 1967 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781719882446 Total Pages :28 pages Book Rating :4.8/5 (824 download)
Book Synopsis Cold-Air Performance of a 12.766-Centimeter-Tip-Diameter Axial-Flow Cooled Turbine. 3: Effect of Rotor Tip Clearance on Overall Performance of a Solid by : National Aeronautics and Space Adm Nasa
Download or read book Cold-Air Performance of a 12.766-Centimeter-Tip-Diameter Axial-Flow Cooled Turbine. 3: Effect of Rotor Tip Clearance on Overall Performance of a Solid written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-08-25 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two tip clearance configurations, one with a recess in the casing and the other with a reduced rotor blade height, were investigated at design equivalent speed over a range of tip clearance from about 2.0 to 5.0 percent of the stator blade height. The optimum configuration with a recess in the casing was the one where the rotor tip diameter was equal to the stator tip diameter (zero blade extension). For this configuration there was an approximate 1.5 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height. For the reduced blade height configurations there was an approximate 2.0 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height. Haas, J. E. and Kofskey, M. G. Glenn Research Center NASA-TP-1032, E-9181 RTOP 505-04
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723249952 Total Pages :26 pages Book Rating :4.2/5 (499 download)
Book Synopsis Cold-Air Performance of a 12.766-Centimeter-Tip-Diameter Axial-Flow Cooled Turbine. 3 by : National Aeronautics and Space Administration (NASA)
Download or read book Cold-Air Performance of a 12.766-Centimeter-Tip-Diameter Axial-Flow Cooled Turbine. 3 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-20 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two tip clearance configurations, one with a recess in the casing and the other with a reduced rotor blade height, were investigated at design equivalent speed over a range of tip clearance from about 2.0 to 5.0 percent of the stator blade height. The optimum configuration with a recess in the casing was the one where the rotor tip diameter was equal to the stator tip diameter (zero blade extension). For this configuration there was an approximate 1.5 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height. For the reduced blade height configurations there was an approximate 2.0 percent decrease in total efficiency for an increase in tip clearance of 1 percent of stator blade height. Haas, J. E. and Kofskey, M. G. Glenn Research Center NASA-TP-1032, E-9181 RTOP 505-04
Book Synopsis Cold-air Investigation of First State of 4 1/2-stage, Fan-drive Turbine with Average Stage-loading Factor of 4.66 by : Warren J. Whitney
Download or read book Cold-air Investigation of First State of 4 1/2-stage, Fan-drive Turbine with Average Stage-loading Factor of 4.66 written by Warren J. Whitney and published by . This book was released on 1981 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
