Read Books Online and Download eBooks, EPub, PDF, Mobi, Kindle, Text Full Free.
Investigation Of The Supersonic Through Flow Compressor Concept Volume Ii Analytical And Experimental Investigations Of Supersonic Cascades And Diffusers
Download Investigation Of The Supersonic Through Flow Compressor Concept Volume Ii Analytical And Experimental Investigations Of Supersonic Cascades And Diffusers full books in PDF, epub, and Kindle. Read online Investigation Of The Supersonic Through Flow Compressor Concept Volume Ii Analytical And Experimental Investigations Of Supersonic Cascades And Diffusers ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
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 Technical Abstract Bulletin by : Defense Documentation Center (U.S.)
Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Supersonic Through-flow Compressor Concept. Volume I. Performance Potential and Mechanical Design Study of the Supersonic Inflow Engine by : Robert L. O'Brien
Download or read book Investigation of the Supersonic Through-flow Compressor Concept. Volume I. Performance Potential and Mechanical Design Study of the Supersonic Inflow Engine written by Robert L. O'Brien and published by . This book was released on 1967 with total page 97 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to evaluate the performance potential of the supersonic inflow turbojet engine (SSIFE) utilizing a supersonic through-flow compressor. The engines considered in this study were designed to operate as accelerators at flight Mach numbers up to 3.5 in the 1980 time period. During the preliminary phases of this study, both cruise and the accelerator engines were considered. The program consisted of a preliminary study of compressor and engine configurations, followed by detailed compressor and engine performance investigations. Experimental investigations of supersonic cascade and diffuser performance were also conducted to provide experimental information required to evaluate this concept. Concurrent with this funded program a corporate-sponsored program was also conducted to evaluate the performance potential of supersonic combustion in the SSIFE and to generate a practical mechanical design for this engine. This report is intended to serve as a summary of all of the work performed on the supersonic inflow engine concept. Comparisons were made between the performance and mechanical design of both the SSIFE and an advanced turbojet sized to produce the same transonic thrust. The SSIFE evolved during the design study was 42 percent shorter, had the same frontal area, and approximately 15 percent greater installed weight than the advanced turbojet. The results obtained from component tests of supersonic cascades and the downstream supersonic diffuser were in general agreement with the level of compression system performance estimated for the engine analyses. (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 with total page 994 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book STAR written by and published by . This book was released on 1973 with total page 904 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hydraulic Research in the United States by :
Download or read book Hydraulic Research in the United States written by and published by . This book was released on 1958 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Adm Nasa Publisher :Independently Published ISBN 13 :9781730729843 Total Pages :66 pages Book Rating :4.7/5 (298 download)
Book Synopsis Analytical and Experimental Studies of a Short Compact Subsonic Diffuser for a Two-Dimensional Supersonic Inlet by : National Aeronautics and Space Adm Nasa
Download or read book Analytical and Experimental Studies of a Short Compact Subsonic Diffuser for a Two-Dimensional Supersonic Inlet written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-11-02 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental study of a two-dimensional supersonic inlet with a short compact subsonic diffuser, length to exit diameter (dl/d) ratio of 1.25, was conducted to investigate the impact of the short diffuser on inlet performance at low speeds and to assess the diffuser subsonic performance for a simulated diffuser flow corresponding to high-speed inlet conditions near the design flight Mach number of 2.2. For the low-speed testing, a drooped lip was employed to improve the inlet performance at a high angle of attack. For the simulated high-speed testing, air was blown through slots or discrete nozzles as an active boundary-layer control. The results from the low-speed performance test were compared with the results from a previous test program on the same inlet with a long subsonic diffuser (dl/d = 4.5). The comparison indicates that inlet recovery was not affected by the use of the short diffuser for either the baseline (no droop) or the drooped cowl lip configuration. However, the inlet baseline distortion for the short diffuser configuration was substantially higher than for the long diffuser. A comparison of the two configurations with a 70 deg drooped lip showed no significant difference in distortion. For the portion of the experimental program in which diffuser conditions for high-speed flight were simulated, diffuser-induced flow separation occurred. This separation was predicted from an analytical study that used the Hess potential flow panel method and the Herring two-dimensional boundary-layer analysis computer codes. The flow separated mainly on the diffuser ramp. Subsequent tests in which boundary-control systems were utilized showed that blowing with either slots or discrete nozzles could suppress the flow separation in the short subsonic diffuser, thereby substantially improving the diffuser performance. Iek, Chanthy and Burley, Richard R. and Johns, Albert L. Glenn Research Center...
Book Synopsis Current Hydraulic Laboratory Research in the United States by :
Download or read book Current Hydraulic Laboratory Research in the United States written by and published by . This book was released on 1958 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Air Force Research Resumés written by and published by . This book was released on with total page 572 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1971 with total page 776 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis ASME Transactions by : American Society of Mechanical Engineers
Download or read book ASME Transactions written by American Society of Mechanical Engineers and published by . This book was released on 1959 with total page 1200 pages. Available in PDF, EPUB and Kindle. Book excerpt: Vols. 2, 4-11, 62-68 include the Society's Membership list; v. 55-80 include the Journal of applied mechanics (also issued separately) as contributions from the Society's Applied Mechanics Division.
Book Synopsis Report by : United States. National Bureau of Standards
Download or read book Report written by United States. National Bureau of Standards and published by . This book was released on 1958 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis National Bureau of Standards Miscellaneous Publication by :
Download or read book National Bureau of Standards Miscellaneous Publication written by and published by . This book was released on 1958 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Miscellaneous Publication - National Bureau of Standards by : United States. National Bureau of Standards
Download or read book Miscellaneous Publication - National Bureau of Standards written by United States. National Bureau of Standards and published by . This book was released on 1934 with total page 188 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NBS Special Publication written by and published by . This book was released on 1958 with total page 334 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Paper written by and published by . This book was released on 1994 with total page 536 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch Publisher : ISBN 13 : Total Pages :1080 pages Book Rating :4.E/5 ( download)
Book Synopsis Japanese Science and Technology, 1983-1984 by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Download or read book Japanese Science and Technology, 1983-1984 written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch and published by . This book was released on 1985 with total page 1080 pages. Available in PDF, EPUB and Kindle. Book excerpt:
