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On The Losses In Convergent Nozzles
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Book Synopsis On the Losses in Convergent Nozzles by : Alexander L. Mellanby
Download or read book On the Losses in Convergent Nozzles written by Alexander L. Mellanby and published by . This book was released on 1921 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis On the Losses in Convergent Nozzles (Classic Reprint) by : A. L. Mellanby
Download or read book On the Losses in Convergent Nozzles (Classic Reprint) written by A. L. Mellanby and published by Forgotten Books. This book was released on 2017-12-23 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: Excerpt from On the Losses in Convergent Nozzles In illustration, Fig. 1 gives a few such curves and, while it indicates differences between the various experimental results, it shows very clearly the peculiarity referred to. The curves for saturated steam flow in straight convergent nozzles show the feature of excessive discharge by rising to values above unity towards the critical range; but, even with this effect, the curve forms are of the same general type as for superheated Steam, where such an influence is absent. About the Publisher Forgotten Books publishes hundreds of thousands of rare and classic books. Find more at www.forgottenbooks.com This book is a reproduction of an important historical work. Forgotten Books uses state-of-the-art technology to digitally reconstruct the work, preserving the original format whilst repairing imperfections present in the aged copy. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in our edition. We do, however, repair the vast majority of imperfections successfully; any imperfections that remain are intentionally left to preserve the state of such historical works.
Book Synopsis On the Losses in Convergent Nozzles by : Alexander L. Mellanby
Download or read book On the Losses in Convergent Nozzles written by Alexander L. Mellanby and published by Palala Press. This book was released on 2016-05-12 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Book Synopsis A Theoretical and Experimental Investigation of the Angularity Loss for Short Convergent-divergent Nozzles with Small Expansion Ratios by : Daniel John Lahti
Download or read book A Theoretical and Experimental Investigation of the Angularity Loss for Short Convergent-divergent Nozzles with Small Expansion Ratios written by Daniel John Lahti and published by . This book was released on 1970 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Divergence Thrust Loss Calculations for Convergent-divergent Nozzles: Extensions to the Classical Case by :
Download or read book Divergence Thrust Loss Calculations for Convergent-divergent Nozzles: Extensions to the Classical Case written by and published by . This book was released on 1991 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781725722637 Total Pages :34 pages Book Rating :4.7/5 (226 download)
Book Synopsis Divergence Thrust Loss Calculations for Convergent-Divergent Nozzles by : National Aeronautics and Space Administration (NASA)
Download or read book Divergence Thrust Loss Calculations for Convergent-Divergent Nozzles written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-17 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: The analytical derivations of the non-axial thrust divergence losses for convergent-divergent nozzles are described as well as how these calculations are embodied in the Navy/NASA engine computer program. The convergent-divergent geometries considered are simple classic axisymmetric nozzles, two dimensional rectangular nozzles, and axisymmetric and two dimensional plug nozzles. A simple, traditional, inviscid mathematical approach is used to deduce the influence of the ineffectual non-axial thrust as a function of the nozzle exit divergence angle. Berton, Jeffrey J. Glenn Research Center NASA-TM-105176, E-6472, NAS 1.15:105176 RTOP 537-01-22...
Book Synopsis Investigation of Convergent-divergent Nozzles Applicable to Reduced-power Supersonic Cruise Aircraft by : Booby L. Berrier
Download or read book Investigation of Convergent-divergent Nozzles Applicable to Reduced-power Supersonic Cruise Aircraft written by Booby L. Berrier and published by . This book was released on 1980 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Convergent-divergent Nozzles Applicable to Reduced-power Supersonic Cruise Aircraft by : Bobby L. Berrier
Download or read book Investigation of Convergent-divergent Nozzles Applicable to Reduced-power Supersonic Cruise Aircraft written by Bobby L. Berrier and published by . This book was released on 1980 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Accurate Determination of the Energy Losses in Convergent Steam Nozzles by : T. A. Worsdell
Download or read book The Accurate Determination of the Energy Losses in Convergent Steam Nozzles written by T. A. Worsdell and published by . This book was released on 1923 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Cold-air Investigation of Three Variable-throat-area Convergent-divergent Nozzles by : John E. McAulay
Download or read book Cold-air Investigation of Three Variable-throat-area Convergent-divergent Nozzles written by John E. McAulay and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Thrust of an Annular Nozzle with a Concave Central Base by : Blake W. Corson (Jr)
Download or read book Static Thrust of an Annular Nozzle with a Concave Central Base written by Blake W. Corson (Jr) and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A static test of an annular nozzle with a concave central base, producing a jet in which tangents to the jet streamlines at the exit converged toward a region on the axis of symmetry downstream of the exit, has indicated good thrust performance. A value of nozzle-flow coefficient only slightly less than unity indicates the internal loss to be small. Pressures on the concave central base are relatively large and positive, and a predictable portion of the total thrust of the jet is exerted on the central base.
Book Synopsis Static Investigation of a Two-dimensional Convergent-divergent Exhaust Nozzle with Multiaxis Thrust-vectoring Capability by : John Gordon Taylor
Download or read book Static Investigation of a Two-dimensional Convergent-divergent Exhaust Nozzle with Multiaxis Thrust-vectoring Capability written by John Gordon Taylor and published by . This book was released on 1990 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Steam Turbines by : William John Goudie
Download or read book Steam Turbines written by William John Goudie and published by . This book was released on 1922 with total page 896 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Compressible Fluid Flow by : P. H. Oosthuizen
Download or read book Compressible Fluid Flow written by P. H. Oosthuizen and published by . This book was released on 1997 with total page 548 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1975 with total page 826 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723469879 Total Pages :112 pages Book Rating :4.4/5 (698 download)
Book Synopsis Two-Dimensional Converging-Diverging Rippled Nozzles at Transonic Speeds. Performed in the Langley 16-Foot Transonic Tunnel by : National Aeronautics and Space Administration (NASA)
Download or read book Two-Dimensional Converging-Diverging Rippled Nozzles at Transonic Speeds. Performed in the Langley 16-Foot Transonic Tunnel written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-23 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was performed in the Langley 16-Foot Transonic tunnel to determine the effects of external and internal flap rippling on the aerodynamics of a nonaxisymmetric nozzle. Data were obtained at several Mach numbers from static conditions to 1.2 over a range of nozzle pressure ratios. Nozzles with chordal boattail angles of 10, 20, and 30 degrees, with and without surface rippling, were tested. No effect on discharge coefficient due to surface rippling was observed. Internal thrust losses due to surface rippling were measured and attributed to a combination of additional internal skin friction and shock losses. External nozzle drag for the baseline configurations were generally less than that for the rippled configurations at all free-stream Mach numbers tested. The difference between the baseline and rippled nozzle drag levels generally increased with increasing boat tail angle. The thrust-minus-drag level for each rippled nozzle configuration was less than the equivalent baseline configuration for each Mach number at the design nozzle pressure ratio. Carlson, John R. and Asbury, Scott C. Langley Research Center CONVERGENT-DIVERGENT NOZZLES; DISCHARGE COEFFICIENT; DRAG; NOZZLE FLOW; NOZZLE GEOMETRY; THRUST; TRAILING EDGES; TRANSONIC SPEED; WIND TUNNEL TESTS; ANGLE OF ATTACK; BOATTAILS; INTERNAL FRICTION; MACH NUMBER; PRESSURE RATIO; SEPARATED FLOW; SKIN FRICTION...
Book Synopsis Investigation of Installation Effects on Single-engine Convergent-divergent Nozzles by : James R. Burley
Download or read book Investigation of Installation Effects on Single-engine Convergent-divergent Nozzles written by James R. Burley and published by . This book was released on 1982 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt: