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Computation Of The Transonic Flow About A Swept Wing In The Presence Of An Engine Nacelle
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Book Synopsis Computation of the Transonic Flow about a Swept Wing in the Presence of an Engine Nacelle by : David S. Ross
Download or read book Computation of the Transonic Flow about a Swept Wing in the Presence of an Engine Nacelle written by David S. Ross and published by Palala Press. This book was released on 2018-03 with total page 192 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 Computation of the Transonic Flow About a Swept Wing in the Presence of an Engine Nacelle (Classic Reprint) by : D. Ross
Download or read book Computation of the Transonic Flow About a Swept Wing in the Presence of an Engine Nacelle (Classic Reprint) written by D. Ross and published by Forgotten Books. This book was released on 2016-09-02 with total page 198 pages. Available in PDF, EPUB and Kindle. Book excerpt: Excerpt from Computation of the Transonic Flow About a Swept Wing in the Presence of an Engine Nacelle A principal goal of computational transonic aerodynamics is to develop computa tional methods for the analysis of transonic flows and for the design of efficient transonic air craft. We are interested in particular in the problem of designing wings with only weak shocks at a given Mach number and angle of attack. Methods, which we shall describe below, exist for the design of shockless transonic airfoils and for computing the transonic ow about a given wing. One approach to the design of a low drag transonic swept wing is to start with a shockiess airfoil in each wing section. Three-dimensional effects will cause shocks on such a wing, but we expect them not to be too severe. By small readjustments of the wing surface, which can be made by a code which treats the wing surface as a free boun dary, we can redesign the wing to reduce the strength of the shocks. Our method takes this program one step further. If an obstacle, such as an engine nacelle, is placed in the ow near an almost shockless wing, sizeable shocks can be expected to appear on the wing. We have incorporated a model of such an obstacle into the free boundary design code of Bauer. 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 Computation of the Transonic Flow about a Swept Wing in the Presence of an Engine Nacelle... by : David S. Ross
Download or read book Computation of the Transonic Flow about a Swept Wing in the Presence of an Engine Nacelle... written by David S. Ross and published by Hardpress Publishing. This book was released on 2013-12 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt: Unlike some other reproductions of classic texts (1) We have not used OCR(Optical Character Recognition), as this leads to bad quality books with introduced typos. (2) In books where there are images such as portraits, maps, sketches etc We have endeavoured to keep the quality of these images, so they represent accurately the original artefact. Although occasionally there may be certain imperfections with these old texts, we feel they deserve to be made available for future generations to enjoy.
Book Synopsis Calculus of Variations and Partial Differential Equations by : Stefan Hildebrandt
Download or read book Calculus of Variations and Partial Differential Equations written by Stefan Hildebrandt and published by Springer. This book was released on 2006-11-14 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
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Book Synopsis Computational Fluid Dynamics Techniques by : Fathi Habashi
Download or read book Computational Fluid Dynamics Techniques written by Fathi Habashi and published by CRC Press. This book was released on 1995-11-22 with total page 930 pages. Available in PDF, EPUB and Kindle. Book excerpt: First published in 1995. Routledge is an imprint of Taylor & Francis, an informa company.
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Book Synopsis On the Numerical Simulation of Three-dimensional Transonic Flow with Application to the C-141 Wing by : Harvard Lomax
Download or read book On the Numerical Simulation of Three-dimensional Transonic Flow with Application to the C-141 Wing written by Harvard Lomax and published by . This book was released on 1973 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results computed by a finite-difference, relaxation algorithm are presented for the supercritical flow (M = 0.825) about the C-141 airplane wing, which has sweep, taper, and twist. Comparisons with both wind-tunnel and flight data indicate that computed solutions of the classical transonic small disturbance equation can accurately simulate high Reynolds number flows when the shock sweep angle is small. It is also shown that this equation poorly approximates the complete potential equation when embedded shock waves are swept at angles greater than about 15 deg. Hence, a more consistent small disturbance equation is derived for use in more general cases.
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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 261) by :
Download or read book Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 261) written by and published by . This book was released on 1991 with total page 566 pages. Available in PDF, EPUB and Kindle. Book excerpt:
