The digital edition of all books may be viewed on our website before purchase. Excerpt from An Artificial Viscosity Method for the Design of Supercritical Airfoils
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Vendeur : Forgotten Books, London, Royaume-Uni
Paperback. Etat : 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. N° de réf. du vendeur 9781334015663_0
Quantité disponible : Plus de 20 disponibles
Vendeur : PBShop.store US, Wood Dale, IL, Etats-Unis
PAP. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur LW-9781334015663
Quantité disponible : 15 disponible(s)
Vendeur : PBShop.store UK, Fairford, GLOS, Royaume-Uni
PAP. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur LW-9781334015663
Quantité disponible : 15 disponible(s)