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Numerical Computation of Hypersonic Flow Past a Two-Dimensional Blunt Body (Classic Reprint) - Tapa blanda
Sinopsis
Excerpt from Numerical Computation of Hypersonic Flow Past a Two-Dimensional Blunt Body
3. Shock Conditions and Initial Conditions Complex Extension Applied to Equations in Characteristic Normal Form.
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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.
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Excerpt from Numerical Computation of Hypersonic Flow Past a Two-Dimensional Blunt Body
3. Shock Conditions and Initial Conditions Complex Extension Applied to Equations in Characteristic Normal Form.
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.
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Excerpt from Numerical Computation of Hypersonic Flow Past a Two-Dimensional Blunt Body
Given a two-dimensional blunt body in a steady supersonic flow of compressible fluid, the problem is to study the flow between the body and the detached shock wave formed in front of it. In this paper, the shock shape is assumed to be analytic and we use it as an initial line in solving a Cauchy problem for the flow and the body. Hyperboliclty of the partial differential equations of motion is achieved in the subsonic region by means of complex extension on one of the independent variables. By means of such a substitution the first order system of nonlinear equations in two dimensions is transformed into a symmetric hyperbolic system in three independent variables. Such an increase in the number of independent variables can be avoided if the equations are written in normal form with respect to two characteristic coordinates. Difference Schemes of second order accuracy are derived for both formulations of the complex extension and they are programmed for the IBM 7090. Five digit accuracy is obtained in the solution and numerical results are presented for a particular flow at Mach 6. The relative merits of the two formulations are discussed.
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.
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Numerical Computation of Hypersonic Flow Past a TwoDimensional Blunt Body Classic Reprint
Librería: PBShop.store US, Wood Dale, IL, Estados Unidos de America
Calificación del vendedor: 5 de 5 estrellas
PAP. Condición: New. New Book. Shipped from UK. Established seller since 2000. Nº de ref. del artículo: LW-9781332170517
Cantidad disponible: 15 disponibles
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Numerical Computation of Hypersonic Flow Past a TwoDimensional Blunt Body Classic Reprint
Librería: PBShop.store UK, Fairford, GLOS, Reino Unido
Calificación del vendedor: 5 de 5 estrellas
PAP. Condición: New. New Book. Shipped from UK. Established seller since 2000. Nº de ref. del artículo: LW-9781332170517
Cantidad disponible: 15 disponibles
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Numerical Computation of Hypersonic Flow Past a Two-Dimensional Blunt Body
Impresión bajo demandaLibrería: Forgotten Books, London, Reino Unido
Calificación del vendedor: 5 de 5 estrellas
Paperback. Condición: New. Print on Demand. This book delves into the complex world of supersonic flow past blunt bodies, an area of great importance in understanding phenomena such as the shockwaves created by supersonic aircraft. The author presents a detailed analysis of the mathematical equations that govern such flows, offering a comprehensive treatment of the Cauchy problem for the flow and body. Notably, the book employs complex extension and difference schemes to derive numerical solutions to the equations, a significant contribution to the field. The author's work provides a solid foundation for further research in supersonic flows and expands our understanding of the intricate interactions between shockwaves and blunt bodies. 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. Nº de ref. del artículo: 9781332170517_0
Cantidad disponible: Más de 20 disponibles