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Test Of A Supersonic Compressor Cascade Vol 2
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Book Synopsis Test of a Supersonic Compressor Cascade (Vol. 2) by : R. L. Holtman
Download or read book Test of a Supersonic Compressor Cascade (Vol. 2) written by R. L. Holtman and published by . This book was released on 1972 with total page 309 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes in detail the experimental investigation of a stationary, linear, supersonic compressor blade cascade. The cascade incorporated contoured sidewalls to control the change in stream-tube area in the quasi-axial direction. The blades had a constant spanwise geometry. The selected blade element was from a recent compressor configuration resulting from the Aerospace Research Laboratories supersonic axial compressor research program. The investigation covered a range of inlet relative Mach numbers of 1.40 - 1.50 and a range of static pressure ratios of approximately 1.5 - 2.1. Volume I describes the cascade design, instrumentation, data reduction techniques, test results, and correlation of results with design characteristics. Volume 2 describes additional work with vortex generators mounted on the blades and compares these results with the plain blade results.
Book Synopsis Test of a Supersonic Compressor Cascade by : Robert L. Holtman
Download or read book Test of a Supersonic Compressor Cascade written by Robert L. Holtman and published by . This book was released on 1972 with total page 323 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes in detail the experimental investigation of a stationary, linear, supersonic compressor blade cascade. The cascade incorporated contoured sidewalls to control the change in stream-tube area in the quasi-axial direction. The blades had a constant spanwise geometry. The selected blade element was from a recent compressor configuration resulting from the Aerospace Research Laboratories supersonic axial compressor research program. The investigation covered a range of inlet relative Mach numbers of 1.40 - 1.50 and a range of static pressure ratios of approximately 1.5 - 2.1. Volume I describes the cascade design, instrumentation, data reduction techniques, test results, and correlation of results with design characteristics. Volume 2 describes additional work with vortex generators mounted on the blades and compares these results with the plain blade results. (Author).
Book Synopsis Test of a Supersonic Compressor Cascade (Vol. 1) by : R. L. Holtman
Download or read book Test of a Supersonic Compressor Cascade (Vol. 1) written by R. L. Holtman and published by . This book was released on 1972 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report describes in detail the experimental investigation of a stationary, linear, supersonic compressor blade cascade. The cascade incorporated contoured sidewalls to control the change in stream-tube area in the quasi-axial direction. The blades had a constant spanwise geometry. The selected blade element was from a recent compressor configuration resulting from the Aerospace Research Laboratories supersonic axial compressor research program. The investigation covered a range of inlet relative Mach numbers of 1.40 - 1.50 and a range of static pressure ratios of approximately 1.5 - 2.1. Volume I describes the cascade design, instrumentation, data reduction techniques, test results, and correlation of results with design characteristics.
Book Synopsis Supersonic Axial Velocity Compressor Study. Volume Iv. Two-dimensional Cascade Test Results by : F. W. Lipfert
Download or read book Supersonic Axial Velocity Compressor Study. Volume Iv. Two-dimensional Cascade Test Results written by F. W. Lipfert and published by . This book was released on 1967 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume presents a description of the cascade tests conducted to establish feasibility of the supersonic axial velocity compressor concept. Two series of tests were conducted at a free stream Mach number of 2.7 using a cascade of four two-dimensional impulse blades, having about 60 deg. turning. The blade profile was modified slightly for the second test series to alleviate suction surface boundary layer separation. The angle of attack of the cascade was varied roughly plus or minus 15 deg. Measurements consisted of pressure distributions along the blade surfaces and the total pressure recovery at the passage exit. The maximum mass-weighted recovery was 80%. (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 1994 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Supersonic Through-flow Compressor Concept. Volume Ii. Analytical and Experimental Investigations of Supersonic Cascades and Diffusers by : Stuart E. Gadbois
Download or read book Investigation of the Supersonic Through-flow Compressor Concept. Volume Ii. Analytical and Experimental Investigations of Supersonic Cascades and Diffusers written by Stuart E. Gadbois and published by . This book was released on 1967 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt: An analytical and experimental investigation of supersonic cascades and supersonic diffusers having entrance conditions representative of the flow discharging from a supersonic through-flow compressor was conducted. The performance of these cascades was predicted over a range of operating conditions using a one-dimensional analysis which included shock and friction losses. Cascade configurations designed to provide up to 65 deg of total turning were tested at supersonic approach Mach numbers over a range of incidence angles. The experimental results were in general agreement with the theoretical performance predicted by the one-dimensional analysis. The test results indicate that rotor efficiencies on the order of 80 percent can be obtained with a supersonic through-flow compressor. A theoretical analysis of the supersonic diffuser was conducted to evaluate the effects of diffuser geometry, bleed flow ratio, and entrance Mach number on the diffuser pressure recovery. Tests of an annular diffuser model ingesting supersonic flows with various amounts of wakes, swirl and boundary layer were conducted. The experimental results showed these flows can be diffused with a process efficiency greater than 90 percent. (Author).
Book Synopsis Government Reports Announcements by :
Download or read book Government Reports Announcements written by and published by . This book was released on 1973-04-25 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Modern Methods of Testing Rotating Components of Turbomachines Instrumentation by : Marc Pianko
Download or read book Modern Methods of Testing Rotating Components of Turbomachines Instrumentation written by Marc Pianko and published by . This book was released on 1975 with total page 210 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Engineering written by and published by . This book was released on 1988 with total page 518 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1989 with total page 1458 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Government Reports Index written by and published by . This book was released on 1975 with total page 908 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 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1982 with total page 310 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Model Research, the National Advisory Committee for Aeronautics, 1915-1958, Volume 2 by : Alex Roland
Download or read book Model Research, the National Advisory Committee for Aeronautics, 1915-1958, Volume 2 written by Alex Roland and published by . This book was released on 1985 with total page 424 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1 by : William R. Hawthorne
Download or read book Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1 written by William R. Hawthorne and published by Princeton University Press. This book was released on 2017-03-14 with total page 647 pages. Available in PDF, EPUB and Kindle. Book excerpt: Volume X of the High Speed Aerodynamics and Jet Propulsion series. Contents include: Theory of Two-Dimensional Flow through Cascades; Three-Dimensional Flow in Turbomachines; Experimental Techniques; Flow in Cascades; The Axial Compressor Stage; The Supersonic Compressor; Aerodynamic Design of Axial Flow Turbines; The Radial Turbine; The Centrifugal Compressor; Intermittent Flow Effects. Originally published in 1964. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Download or read book NASA SP. written by and published by . This book was released on 1988 with total page 624 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Compressors written by and published by . This book was released on 1988 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:
