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).
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).
Download or read book Interference Problems on Wing fuselage Combinations in Inviscid Incompressible Flow written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1974 with total page 1212 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1981 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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).
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 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).
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).
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).
Download or read book Government reports annual index written by and published by . This book was released on 199? with total page 1362 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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).
Download or read book Government Reports Announcements Index written by and published by . This book was released on 1983 with total page 944 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
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.
Download or read book Government Reports Annual Index Keyword A L written by and published by . This book was released on 1983 with total page 1216 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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).
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:
