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Hardback or Cased Book. Condizione: New. An Artificial Viscosity Method for the Design of Supercritical Airfoils. Book.

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Taschenbuch. Condizione: Neu. Neuware - This technical report details an artificial viscosity method for designing supercritical airfoils. The method provides a way to compute shock-free airfoils, addressing a key challenge in high-speed aerodynamics. The report presents the mathematical formulation and numerical implementation of the artificial viscosity technique, highlighting its application to airfoil design. This study offers insights into computational fluid dynamics and airfoil optimization, making it a valuable resource for engineers and researchers in aerospace and related fields.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.…

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Paperback. Condizione: New. Print on Demand. This book presents a numerical technique to design supercritical airfoils for increased efficiency in aircraft performance. Developed from computational transonic aerodynamics, the method outlined by the author solves the inverse problem of calculating the shape an airfoil must have in order to achieve a specified pressure distribution. The book includes descriptions of pressure distributions that generate airfoils with low wave drag, and indicates how to modify the input distribution in order to obtain airfoils with a desired lift, thickness to -chord ratio, and design Mach number. The author provides a convergence proof for the design problem in a special case of subsonic flow, and a description of the modified version of the Bauer, Garabedian, and Korn analysis code H, which is used to perform the flow calculations. Through the use of artificial viscosity, the author shows that it is possible to obtain wing sections with low wave drag by using the technique described in this book. This book is a reproduction of an important historical work, digitally reconstructed using state-of-the-art technology to preserve the original format. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in the book. print-on-demand item.…

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Buch. Condizione: Neu. Neuware - This technical report details an artificial viscosity method for designing supercritical airfoils. The method provides a way to compute shock-free airfoils, addressing a key challenge in high-speed aerodynamics. The report presents the mathematical formulation and numerical implementation of the artificial viscosity technique, highlighting its application to airfoil design. This study offers insights into computational fluid dynamics and airfoil optimization, making it a valuable resource for engineers and researchers in aerospace and related fields.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.…

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Taschenbuch. Condizione: Neu. Druck auf Anfrage Neuware - Printed after ordering - This IMA Volume in Mathematics and its Applications ON THE EVOLUTION OF PHASE BOUNDARIES is based on the proceedings of a workshop which was an integral part of the 1990- 91 IMA program on 'Phase Transitions and Free Boundaries'. The purpose of the workshop was to bring together mathematicians and other scientists working on the Stefan problem and related theories for modeling physical phenomena that occurs in two phase systems. We thank M.E. Gurtin and G. McFadden for editing the proceedings. We also take this opportunity to thank the National Science Foundation, whose financial support made the workshop possible. A vner Friedman Willard Miller, Jr. PREFACE A primary goal of the IMA workshop on the Evolution of Phase Boundaries from September 17-21, 1990 was to emphasize the interdisciplinary nature of contempo rary research in this field, research which combines ideas from nonlinear partial dif ferential equations, asymptotic analysis, numerical computation, and experimental science. The workshop brought together researchers from several disciplines, includ ing mathematics, physics, and both experimental and theoretical materials science.…