Geoffrey b mcfadden (42 risultati)

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

Condizione: New.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

hardcover. Condizione: Very Good. Fast Shipping - Safe and Secure 7 days a week.

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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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HRD. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

Condizione: As New. Unread book in perfect condition.

HRD. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

HRD. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

HRD. Condizione: New. New Book. Shipped from UK. Established seller since 2000.

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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.…

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.…

Condizione: New. KlappentextrnrnUnlike 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, sketc.

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.…

Condizione: As New. Unread book in perfect condition.

Condizione: New. In English.

Condizione: New.

Condizione: New.

Condizione: As New. Unread book in perfect condition.

Condizione: New. pp. 156.