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Investigation Of A High Through Flow Single Stage Axial Flow Compressor With Tip Clearance Increased 0020 Inch And Casing Vortex Generator Configuration B Configuration 3b
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Book Synopsis Investigation of A High-through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch and Casing Vortex Generator Configuration B (Configuration 3B). by : C. Herbert Law
Download or read book Investigation of A High-through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch and Casing Vortex Generator Configuration B (Configuration 3B). written by C. Herbert Law and published by . This book was released on 1981 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Complete experimental results are presented from tests of an axial compressor with casing vortex generators. The design objectives were for a flow per unit frontal area of 39.7 lb/sec/sq ft, a total pressure ratio of 1.912 and a tip speed of 1500 ft/sec. These experimental results were achieved with one of a series of minor parametric modifications to the baseline compressor stage. No conclusions concerning the effects of these modifications will be drawn until the complete series of tests has been reported. (Author).
Book Synopsis Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.010 Inch and Casing Vortex Generator Configuration B (Configuration 2B). by : C. Herbert Law
Download or read book Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.010 Inch and Casing Vortex Generator Configuration B (Configuration 2B). written by C. Herbert Law and published by . This book was released on 1981 with total page 103 pages. Available in PDF, EPUB and Kindle. Book excerpt: Complete experimental results are presented from tests of an axial compressor with casing vortex generators. The design objectives were for a flow per unit frontal area of 39.7 pounds per second per square feet, a total pressure ratio of 1.912 and a tip speed of 1500 feet per second. These experimental results were achieved with one of a series of minor parametric modifications to the baseline compressor stage. No conclusions concerning the effects of these modifications will be drawn until the complete series of tests has been reported. (Author).
Book Synopsis Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch and Casing Vortex Generator Configuration A (Configuration 3A). by : C. Herbert Law
Download or read book Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch and Casing Vortex Generator Configuration A (Configuration 3A). written by C. Herbert Law and published by . This book was released on 1981 with total page 95 pages. Available in PDF, EPUB and Kindle. Book excerpt: Complete experimental results are presented from tests of an axial compressor with casing vortex generators. The design objectives were for a flow per unit frontal area of 39.7 pounds per second per square feet, a total pressure ratio of 1.912 and a tip speed of 1500 feet per second. These experimental results were achieved with one of a series of minor parametric modifications to the baseline compressor stage. No conclusions concerning the effects of these modifications will be drawn until the complete series of tests has been reported. (Author).
Book Synopsis Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch and Casing Vortex Generator Configuration 'C' (Configuration 3C). by : C. Herbert Law
Download or read book Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch and Casing Vortex Generator Configuration 'C' (Configuration 3C). written by C. Herbert Law and published by . This book was released on 1981 with total page 101 pages. Available in PDF, EPUB and Kindle. Book excerpt: Complete experimental results are presented from tests of an axial compressor with casing vortex generators. The design objectives were for a flow per unit frontal area of 39.7 lb/sec/ft2, a total pressure ratio of 1.912 and a tip speed of 1500 ft/sec. These experimental results were achieved with one of a series of minor parametric modifications to the baseline compressor stage. No conclusions concerning the effects of these modifications will be drawn until the complete series of tests has been reported. (Author).
Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1981 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.010 Inch and Casing Vortex Generator Configuration A (Configuration 2A). by : C. Herbert Law
Download or read book Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.010 Inch and Casing Vortex Generator Configuration A (Configuration 2A). written by C. Herbert Law and published by . This book was released on 1981 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt: Complete experimental results are presented from tests of an axial compressor with casing vortex generators. The design objectives were for a flow per unit frontal area of 39.7 lb/sec/sq. ft., a total pressure ratio of 1.912 and a tip speed of 1500 ft/sec. These experimental results were achieved with one of a series of minor parametric modifications to the baseline compressor stage. No conclusions concerning the effects of these modifications will be drawn until the complete series of tests has been reported. (Author).
Book Synopsis Investigation of a High-Through Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased O.010 Inch and Casing Vortex Generator Configuration 'C' (Configuration 2C). by : C. Herbert Law
Download or read book Investigation of a High-Through Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased O.010 Inch and Casing Vortex Generator Configuration 'C' (Configuration 2C). written by C. Herbert Law and published by . This book was released on 1981 with total page 103 pages. Available in PDF, EPUB and Kindle. Book excerpt: Complete experimental results are presented from tests of an axial compressor with casing vortex generators. The design objectives were for a flow per unit frontal area of 39.7 lb/sec/sq ft, a total pressure ratio of 1.912 and a tip speed of 1500 ft/sec. These experimental results were achieved with one of a series of minor parametric modifications to the baseline compressor stage. No conclusions concerning the effects of these modifications will be drawn until the complete series of tests has been reported. (Author).
Book Synopsis Investigation of a High-through-Flow Single-Stage, Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch, Rotor Tip Vortex Generators, and Casing Vortex Generators Configuration B, Configuration 3.1.B. by : Arthur J. Wennerstrom
Download or read book Investigation of a High-through-Flow Single-Stage, Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch, Rotor Tip Vortex Generators, and Casing Vortex Generators Configuration B, Configuration 3.1.B. written by Arthur J. Wennerstrom and published by . This book was released on 1982 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt: Complete experimental results are presented from tests of an axial compressor combining both rotor-mounted and casing-mounted vortex generators. The design objectives were for a flow per unit frontal area of 39.7 lb/sec/sq.ft., a total pressure ratio of 1.912 and a tip speed of 1500 ft/sec. These experimental results were achieved with one of a series of minor parametric modifications to the baseline compressor stage. No conclusions concerning the effects of these modifications will be drawn until the complete series of tests has been reported. (Author).
Book Synopsis Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch and Rotor Tip Vortex Generators, Configuration 3.1 by : Arthur J. Wennerstrom
Download or read book Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch and Rotor Tip Vortex Generators, Configuration 3.1 written by Arthur J. Wennerstrom and published by . This book was released on 1982 with total page 119 pages. Available in PDF, EPUB and Kindle. Book excerpt: Complete experimental results are presented from tests of an axial compressor with rotor-mounted vortex generators. The design objectives were for a flow per unit frontal area of 39.7 1b/sec sq. ft., a total pressure ratio of 1.912 and a tip spread of 1500 ft/sec. These experimental results were achieved with one of a series of minor parametric modifications to the baseline compressor stage. No conclusions concerning the effects of these modifications will be drawn until the complete series of tests has been reported. (Author).
Book Synopsis Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Casing Vortex Generator Configuration 'B' (Configuration 1B). by : Arthur J. Wennerstrom
Download or read book Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Casing Vortex Generator Configuration 'B' (Configuration 1B). written by Arthur J. Wennerstrom and published by . This book was released on 1980 with total page 105 pages. Available in PDF, EPUB and Kindle. Book excerpt: For abstract see AD B050 857L.
Book Synopsis Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.010 Inch (Configuration 2). by : C. Herbert Law
Download or read book Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.010 Inch (Configuration 2). written by C. Herbert Law and published by . This book was released on 1981 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of an experimental evaluation of the single-stage axial compressor with tip clearance increased 0.010 inch. This clearance increase was accomplished by grinding this amount off the tips of the rotor blades. The casing was untouched. The performance goals of this stage were based on a preliminary design study of a multi-stage compressor for an advanced turbojet engine. The results of the tests, reported herein, were achieved with one of a series of minor parametric modifications to the compressor stage. The parametric modifications considered consisted of three casing vortex generator configurations, three separate rotor tip running clearances, and one rotor tip vortex generator configuration. No casing or rotor tip vortex generators were used on the configuration reported herein.
Book Synopsis Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch (Configuration 3). by : C. Herbert Law
Download or read book Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Tip Clearance Increased 0.020 Inch (Configuration 3). written by C. Herbert Law and published by . This book was released on 1981 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: Complete experimental results are presented from tests of an axial compressor. The design objectives were for a flow per unit frontal area of 39.7 lb/sec/sq ft, a total pressure ratio of 1.912 and a tip speed of 1500 ft/sec. These experimental results were achieved with one of a series of minor parametric modifications to the baseline compressor stage. No conclusions concerning the effects of these modifications will be drawn until the complete series of tests has been reported. (Author).
Book Synopsis Effects of Inlet-guide-vane Configuration and Relative Blade Velocity on Noise from Axial-flow Compressors by : David Chestnutt
Download or read book Effects of Inlet-guide-vane Configuration and Relative Blade Velocity on Noise from Axial-flow Compressors written by David Chestnutt and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Design and Tests of a Six-stage Axial-flow Compressor Having a Tip Speed of 550 Feet Per Second and a Flat Operating Characteristic at Constant Speed by : Willard R. Westphal
Download or read book Design and Tests of a Six-stage Axial-flow Compressor Having a Tip Speed of 550 Feet Per Second and a Flat Operating Characteristic at Constant Speed written by Willard R. Westphal and published by . This book was released on 1958 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: A six-stage axial-flow compressor with a tip speed of 550 feet per second and a flat operating characteristics at constant speed has been designed and tested. It was designed for a constant power input per pound of flow in expectation that this would result in a wider mass-flow operating range at a given stagnation-presssure ratio. The design specific weight flow was 21.3 pounds per second per square foot of frontal area at atmospheric discharge with a stagnation-pressure ratio of 3.25 and an inlet hub-tip radius ratio of 0.7. Several configurations consisting of various blade setting angles and solidities were tested. Tests showed that the design flow, pressure ratio, and flat operating characteristic were obtained over a range of 10 percent of design flow at a peak efficiency of 82 percent for design conditions. The compressor had a possible immediate application for air removal from a large slotted-throat transonic wind tunnel, but the design theory could apply to any low-speed industrial compressor or second spool of a turbojet engine.
Book Synopsis Investigation of an Impulse Axial-flow Compressor by : John R. Erwin
Download or read book Investigation of an Impulse Axial-flow Compressor written by John R. Erwin and published by . This book was released on 1950 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Rotating Stall Investigation of the 0.72 Hub-tip Ratio Single-stage Compressor by : Robert W. Graham
Download or read book Rotating Stall Investigation of the 0.72 Hub-tip Ratio Single-stage Compressor written by Robert W. Graham and published by . This book was released on 1954 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of an Impulse Axial-flow Compressor Rotor Over a Range of Blade Angles by : Wallace M. Schulze
Download or read book Investigation of an Impulse Axial-flow Compressor Rotor Over a Range of Blade Angles written by Wallace M. Schulze and published by . This book was released on 1950 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
