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Author : H. Hefazi
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book A Computational Study of Supersonic Impulse Cascade Performance written by H. Hefazi and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
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ISBN 13 :
Total Pages : 974 pages
Book Rating : 4.F/5 ( download)
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 974 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 694 pages
Book Rating : 4.0/5 ( download)
Download or read book 34th Aerospace Sciences Meeting & Exhibit written by and published by . This book was released on 1996 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : George R. Inger
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Analytical and Computational Study of Wall Temperature Jumps in Supersonic Flow written by George R. Inger and published by . This book was released on 1999 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 662 pages
Book Rating : 4.F/5 ( download)
Download or read book Aerospace America written by and published by . This book was released on 1995 with total page 662 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : American Institute of Aeronautics and Astronautics. Technical Information Service
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ISBN 13 :
Total Pages : 184 pages
Book Rating : 4.3/5 (91 download)
Download or read book The Finding Guide to AIAA Meeting Papers written by American Institute of Aeronautics and Astronautics. Technical Information Service and published by . This book was released on 1996 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Sang Y. Han
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Computational Study of Supersonic Jets from Swirl-inducing Nozzles written by Sang Y. Han and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 620 pages
Book Rating : 4.:/5 (31 download)
Download or read book Report written by and published by . This book was released on 1945 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Odus R. Burggraf
Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.:/5 (227 download)
Download or read book Computational Study of Supersonic Flow Over Backward-Facing Steps at High Reynolds Number written by Odus R. Burggraf and published by . This book was released on 1970 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of laminar separated flow over a backward-facing step is solved numerically for the limiting case of infinite Reynolds number. The flow model adopted is that deduced by Batchelor for incompressible flow: an inviscid rotational eddy confined within the recirculation portion of the separated shear layer. It is argued that the reattachment process is essentially inviscid in the limit R approaches infinity, and the flow field in the reattachment zone is computed on this basis. The computed results support Chapman's model of the reattachment process as the correct limit case, to second-order accuracy, as the flow angle entering the reattachment zone approaches zero. For the recirculation zone, the boundary-layer equations are simplified by assuming a constant pressure eddy. The Dorodnitsyn transformation is applied and numerical solutions obtained using an implicit finite-difference scheme. The solutions are carried out from station-to-station in the direction of flow over a complete cycle of recirculation. Iteration yields the unique value of the vorticity in the inviscid layer upstream of separation, including the effects of corner expansion and recirculation on the development of the separated shear layer. (Author).
Author : T. L. Henderson
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Computational Study of the Inviscid, Non-linear Physics of Supersonic Base Flows written by T. L. Henderson and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 1102 pages
Book Rating : 4.X/5 (2 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1991 with total page 1102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Xin Zhang
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book A Computational Analysis of Supersonic Jet and Instability Wave Interaction written by Xin Zhang and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : I. Fruchtman
Publisher :
ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.:/5 (792 download)
Download or read book The Supersonic Turbine written by I. Fruchtman and published by . This book was released on 1971 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 888 pages
Book Rating : 4.:/5 (334 download)
Download or read book STAR written by and published by . This book was released on 1973 with total page 888 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Douglas W. Dusing
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book An Experimental and Computational Study of Unsteady Supersonic 2-D Open Cavity Flow Physics written by Douglas W. Dusing and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 534 pages
Book Rating : 4.:/5 (319 download)
Download or read book Annual Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 534 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert L. O'Brien
Publisher :
ISBN 13 :
Total Pages : 97 pages
Book Rating : 4.:/5 (227 download)
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).
