Unsteady Transonic Flow Past Airfoils in Rigid Body Motion (Classic Reprint) PDF Download
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Author: I. -Chung Chang Publisher: Forgotten Books ISBN: 9780265551530 Category : Science Languages : en Pages : 210
Book Description
Excerpt from Unsteady Transonic Flow Past Airfoils in Rigid Body Motion 1. Characteristic Surface 2. Computational Boundary Conditions 3. Coordinate Transformation Technique. 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.
Author: I. -Chung Chang Publisher: Forgotten Books ISBN: 9780265551530 Category : Science Languages : en Pages : 210
Book Description
Excerpt from Unsteady Transonic Flow Past Airfoils in Rigid Body Motion 1. Characteristic Surface 2. Computational Boundary Conditions 3. Coordinate Transformation Technique. 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.
Author: I-Chung Chang Publisher: Sagwan Press ISBN: 9781377066332 Category : Languages : en Pages : 206
Book Description
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.
Author: Publisher: ISBN: Category : Languages : en Pages : 0
Book Description
A perturbation theory and numerical solution, based on the unsteady full potential equation, were developed to calculate the unsteady transonic flow field over blunt and pointed bodies of revolution performing harmonic oscillatory motions at zero incidence. Calculations were performed for pulsatile oscillations for a hemisphere-cylinder and pitching oscillations for an ogive-cylinder, an ellipse-cylinder, a hemisphere-cylinder, and a parabolic arc nose. Comparison between theory and experiments was made for the surface pressure distribution at quasi-steady state and for the static and dynamic stability derivatives. (Author).
Author: David Nixon Publisher: ISBN: Category : Science Languages : en Pages : 410
Book Description
This volume complements Transonic aerodynamics (v.81 in the series) which is concerned with steady flow. This is the only book to address the subject of unsteady transonic aerodynamics, a field much different from steady aerodynamics. The most pronounced difference is the complex shock wave motions
Author: Antony Jameson Publisher: Cambridge University Press ISBN: 1108837883 Category : Science Languages : en Pages : 627
Book Description
Learn the design and analysis of numerical algorithms for aerodynamics. Ideal for graduates, researchers, and professionals in the field.
Author: I. -Chung Chang
Author: I. -Chung Chang
Author: Chang I. -Chung
Author: I-Chung Chang
Author: 
Author: Mårten Landahl
Author: Liu Gao-lian
Author: Marten Landahl
Author: 
Author: David Nixon
Author: Antony Jameson