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Author : Jain-Ming Wu
Publisher :
ISBN 13 :
Total Pages : 10 pages
Book Rating : 4.:/5 (472 download)
Download or read book Experimental Investigation of Supersonic Flow Separation Over a Rearward Facing Step written by Jain-Ming Wu and published by . This book was released on 1970 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (227 download)
Download or read book SUPERSONIC FLOW SEPARATION ON A BACKWARD FACING STEP. written by and published by . This book was released on 1966 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: The paper describes an experimental survey of flow separation on backward facing steps having different heights at a Mach number of 2.4. Reattachment and critical points are found for three regimes, laminar, transitional, and turbulent. Reattachment occurs at a point where the pressure is 35% of the free stream value for turbulent flow, and 60% of this value in the laminar case. The length of the free shear layer is found to be one-half that of the separating streamline, a result which emphasizes the importance of the reattachment region. The flow downstream of the critical point is found to be relatively independent of the base flow. Disturbances in the spanwise direction are always observed in laminar flow but do not affect the base pressure.
Author : Howard E. Smith
Publisher :
ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.:/5 (183 download)
Download or read book The Flow Field and Heat Transfer Downstream of a Rearward Facing Step in Supersonic Flow written by Howard E. Smith and published by . This book was released on 1967 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Edward Malcolm Harvey Newton
Publisher :
ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (228 download)
Download or read book Experimental Investigation of Supersonic Flow in the Neighborhood of a Forward-facing Step written by Edward Malcolm Harvey Newton and published by . This book was released on 1964 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : G. E. Gadd
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book An Experimental Investigation of Heat Transfer Effects on Boundary Layer Separation in Supersonic Flow written by G. E. Gadd and published by . This book was released on 1956 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Abdallah Antoun Sfeir
Publisher :
ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.:/5 (21 download)
Download or read book Supersonic Flow Separation on a Backward Facing Step written by Abdallah Antoun Sfeir and published by . This book was released on 1966 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael Wen-Shean Su
Publisher :
ISBN 13 :
Total Pages : 142 pages
Book Rating : 4.:/5 (791 download)
Download or read book Investigation of Supersonic Flow Over a Rearward Facing Step written by Michael Wen-Shean Su and published by . This book was released on 1970 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Howard Edwin Smith
Publisher :
ISBN 13 :
Total Pages : 236 pages
Book Rating : 4.:/5 (181 download)
Download or read book Experimental and Theoretical Investigation of the Near Wake Behind a Rearward Facing Step in Supersonic Flow written by Howard Edwin Smith and published by . This book was released on 1969 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
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ISBN 13 :
Total Pages : 1264 pages
Book Rating : 4.3/5 (243 download)
Download or read book OAR Cumulative Index of Research Results written by and published by . This book was released on 1967 with total page 1264 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jean J. Ginoux
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)
Download or read book On the Existence of Cross Flows in Separated Supersonic Streams written by Jean J. Ginoux and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was made on laminar separated supersonic streams using two-dimensional backward-facing step models. It was shown that a cross-flow existed in the separated region of the flow which is associated with the side wall boundary-layers. Its effect is to decrease the base pressure and increase the pressure gradient at reattachment even for large values of the model-span to step-height ratio. It is shown that the commonly accepted assumption that a twodimensional flow exists when there is no measurable spanwise pressure variation is a necessary but not sufficient condition. In the turbulent case, it is generally found that the measured base pressure is lower than is theoretically predicted. This is explained by the existence of a cross-flow (suction) produced by strong vertical vortices near the side walls. (Author).
Author : Donald M. Kuehn
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (461 download)
Download or read book Experimental Investigation of the Pressure Rise Required for the Incipient Separation of Turbulent Boundary Layers in Two-dimensional Supersonic Flow written by Donald M. Kuehn and published by . This book was released on 1959 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Robert Earl Wilson
Publisher :
ISBN 13 :
Total Pages : 110 pages
Book Rating : 4.:/5 (825 download)
Download or read book An Experimental Investigation of Separated Turbulent Supersonic Flow at M written by Robert Earl Wilson and published by . This book was released on 1966 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:
![Download Experimental Investigation of Pressure Rise Required for Incipient Separation of Turbulent Boundary Layers in 2-dimensional Supersonic Flow [with List of References] PDF Online Free](https://books.google.com/books/content/images/frontcover/pCmDswEACAAJ?fife=w200-h370)
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ISBN 13 :
Total Pages : 8 pages
Book Rating : 4.:/5 (979 download)
Download or read book Experimental Investigation of Pressure Rise Required for Incipient Separation of Turbulent Boundary Layers in 2-dimensional Supersonic Flow [with List of References] written by and published by . This book was released on 1959 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
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ISBN 13 :
Total Pages : 912 pages
Book Rating : 4.E/5 ( download)
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 912 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : V. M. Kovalenko
Publisher :
ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.:/5 (227 download)
Download or read book Experimental Investigation of a Turbulent Boundary Layer on a Greatly Elongated Body of Revolution in a Supersonic Flow written by V. M. Kovalenko and published by . This book was released on 1974 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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ISBN 13 :
Total Pages : 238 pages
Book Rating : 4.:/5 (227 download)
Download or read book Experimental Investigation of Supersonic Flows with Separated Regions in Ducts written by and published by . This book was released on 1995 with total page 238 pages. Available in PDF, EPUB and Kindle. Book excerpt: As applied to supersonic diffusers of different purpose and scramjet engines separation flows in various geometry ducts are investigated. Flow Mach and Reynolds numbers at the entrance to the ducts ranged from I to 6 and from 4. IO% to 7.1O%, respectively. The transition from supersonic flow to subsonic flow efficiency defined by the transition region length and pressure recovery. Separated and non- separated flow boundaries are determined. Hydraulic diameter concept expediency for separation flows analysis is appraised. Scramiet separation flows of different kinds were simulated. The influence on separation flows of such factors as off design modes of diffuser, combustors, non-uniformity of flow interaction of separated regions initiated by back pressure, secondary jets, cavities, struts and other kinds of elements of scramjet combustors are investigated. Several methods of separation control promoting flow stabilization and decreasing separated region lengths are offered.
Author : Thomas Johani
Publisher :
ISBN 13 :
Total Pages : 142 pages
Book Rating : 4.:/5 (379 download)
Download or read book An Experimental Investigation of Boundary Layer Expansion Around a Convex Corner in Supersonic Flow written by Thomas Johani and published by . This book was released on 1968 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:
