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Design And Two Dimensional Cascade Test Of Turbine Stator Blade With Ratio Of Axial Chord To Spacing Of 05
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Book Synopsis Design and Two-dimensional Cascade Test of Turbine Stator Blade with Ratio of Axial Chord to Spacing of 0.5 by : Roy G. Stabe
Download or read book Design and Two-dimensional Cascade Test of Turbine Stator Blade with Ratio of Axial Chord to Spacing of 0.5 written by Roy G. Stabe and published by . This book was released on 1970 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design and Two-dimensional Cascade Test of a Jet-flap Turbine Stator Blade with Ratio of Axial Chord to Spacing of 0.5 by : Roy G. Stabe
Download or read book Design and Two-dimensional Cascade Test of a Jet-flap Turbine Stator Blade with Ratio of Axial Chord to Spacing of 0.5 written by Roy G. Stabe and published by . This book was released on 1971 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design and Two-dimensional Cascade Test of Turbine Stator Blade with Ratio of Axial Chord to Spacing of 0.5 by : Roy G. Stabe
Download or read book Design and Two-dimensional Cascade Test of Turbine Stator Blade with Ratio of Axial Chord to Spacing of 0.5 written by Roy G. Stabe and published by . This book was released on 1970 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Turbine Design and Application by : Arthur J. Glassman
Download or read book Turbine Design and Application written by Arthur J. Glassman and published by . This book was released on 1972 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1972 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1972 with total page 958 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 Synopsis Two-dimensional Cascade Investigation of a Turbine Tandem Blade Design by : Stanley M. Nosek
Download or read book Two-dimensional Cascade Investigation of a Turbine Tandem Blade Design written by Stanley M. Nosek and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Trailing Edge Geometry and Thickness on the Performance of Certain Turbine Stator Blading by : Herman W. Prust
Download or read book Effect of Trailing Edge Geometry and Thickness on the Performance of Certain Turbine Stator Blading written by Herman W. Prust and published by . This book was released on 1972 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The experimental and analytical investigation included solid blades with five different trailing-edge thicknesses and four different trailing-edge geometries. One of the geometries was round, one was square, one was tapered from the suction surface, and the other tapered from the pressure surface. One of the trailing-edge thicknesses was sharp edged; the other four thicknesses were equivalent to about 5, 11, 16, and 20 percent of the blade throat width. The experimental results show increased efficiency loss for increased trailing-edge thickness for all trailing-edge geometries. The blade with round trailing edge, equal to about 11 percent of the blade throat width, had 60 percent more loss than the sharp-edged blade. For the same trailing-edge thickness, square trailing edges caused more loss than round trailing edges, and the tapered trailing edges caused about the same loss as the round trailing edges.
Book Synopsis Two-dimensional Cold-air Cascade Study of a Film-cooled Turbine Stator Blade. 5: Comparison of Experimental and Analytical Aerodynamic Results for Blade with 12 Rows of 0.038-centimeter-(0.015 Inch) Diameter Coolant Holes Having Streamwise Ejection Angl by :
Download or read book Two-dimensional Cold-air Cascade Study of a Film-cooled Turbine Stator Blade. 5: Comparison of Experimental and Analytical Aerodynamic Results for Blade with 12 Rows of 0.038-centimeter-(0.015 Inch) Diameter Coolant Holes Having Streamwise Ejection Angl written by and published by . This book was released on 1978 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Two-dimensional Cascade Test of a Jet-flap Turbine Rotor Blade by : John F. Kline
Download or read book Two-dimensional Cascade Test of a Jet-flap Turbine Rotor Blade written by John F. Kline and published by . This book was released on 1971 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781720155133 Total Pages :26 pages Book Rating :4.1/5 (551 download)
Book Synopsis Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 5: Comparison of Experimental and Analytical Aerodynamic Results for Bla by : National Aeronautics and Space Adm Nasa
Download or read book Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 5: Comparison of Experimental and Analytical Aerodynamic Results for Bla written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-10 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Published experimental aerodynamic efficiency results were compared with results predicted from two published analytical methods. This is the second of two such comparisons. One of the analytical methods was used as published; the other was modified for certain cases of coolant discharge from the blade suction surface. The results show that for 23 cases of single row and multirow discharge covering coolant fractions from 0 to about 9 percent, the difference between the experimental and predicted results was no greater than about 1 percent in any case and less than 1/2 percent in most cases. Prust, H. W., Jr. Glenn Research Center NASA-TP-1204, E-9342 RTOP 505-04
Book Synopsis Design and Experimental Results for a Turbine with Jet Flap Stator and Jet Flap by : James L. Bettner
Download or read book Design and Experimental Results for a Turbine with Jet Flap Stator and Jet Flap written by James L. Bettner and published by . This book was released on 1973 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt: The overall performance and detailed stator performance of a negative hub reaction turbine design featuring a moderately low solidity jet flap stator and a jet flap rotor were determined. Testing was conducted over a range of turbine expansion ratios at design speed. At each expansion ratio, the stator jet flow and rotor jet flow ranged up to about 7 and 8 percent, respectively, of the turbine inlet flow. The performance of the jet flap stator/jet flap rotor turbine was compared with that of a turbine which used the same jet flap rotor and a conventional, high solidity plan stator. The effect on performance of increased axial spacing between the jet stator and rotor was also investigated.
Download or read book NASA SP. written by and published by . This book was released on 1982 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723300318 Total Pages :24 pages Book Rating :4.3/5 (3 download)
Book Synopsis Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 5 by : National Aeronautics and Space Administration (NASA)
Download or read book Two-Dimensional Cold-Air Cascade Study of a Film-Cooled Turbine Stator Blade. 5 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 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Published experimental aerodynamic efficiency results were compared with results predicted from two published analytical methods. This is the second of two such comparisons. One of the analytical methods was used as published; the other was modified for certain cases of coolant discharge from the blade suction surface. The results show that for 23 cases of single row and multirow discharge covering coolant fractions from 0 to about 9 percent, the difference between the experimental and predicted results was no greater than about 1 percent in any case and less than 1/2 percent in most cases. Prust, H. W., Jr. Glenn Research Center NASA-TP-1204, E-9342 RTOP 505-04
Book Synopsis Two-dimensional Cold Air Cascade Study of a Film Cooled Turbine Stator Blade by : Herman W. Purst
Download or read book Two-dimensional Cold Air Cascade Study of a Film Cooled Turbine Stator Blade written by Herman W. Purst and published by . This book was released on 1975 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Approximate design method for high-solidity blade elements in compressors and turbines by : John Stanitz
Download or read book Approximate design method for high-solidity blade elements in compressors and turbines written by John Stanitz and published by Рипол Классик. This book was released on 1951 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate blade-element design method is developed for compressible or incompressible nonviscous flow in high-solidity stators or rotors of axial-, radial-, or mixed-flow compressors, turbines, or two-dimensinal cascades. The method is based upon channel-type flow between blade elements on a specified surface of revolution that lies between the hub and shroud (casing) and is concentric with the axis of the compressor turbine. The blade elements is designed for prescribed velocities along the blade-element profile as a function of distance along meridonal lines on the surface of revolution. Two numerical examples are presented: (1) the design of a blade-element profile for a plane two-dimensional cascade in compressible flow with the prescribed velocities along the profiles; and (2) the design of a blade element for the impeller of a mixed-flow centrifugal compressor.
Book Synopsis Experimental Investigation in an Annular Cascade Sector of Highly Loaded Turbine Stator Blading by : James L. Bettner
Download or read book Experimental Investigation in an Annular Cascade Sector of Highly Loaded Turbine Stator Blading written by James L. Bettner and published by . This book was released on 1970 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report investigates testing low reaction jet turbine stator blades in a six-blade annular cascade.
