Computation of Hypersonic Axially Symmetric Flow at Low Mach Numbers (Classic Reprint) - Couverture souple
Synopsis
Explore how complex flow is modeled and solved for axially symmetric bodies at low Mach numbers. This rigorous study presents the mathematical foundation, including the equations of motion and their reduction to a characteristic normal form. It also dives into shock conditions, shock shapes, and how these influence the flow field around a body.
The book explains both two- and three-dimensional approaches, highlighting when real versus complex characteristics occur and how analytic extension helps keep the problem well posed. It discusses the method of characteristics, its numerical implementation, and the challenges of stability and singularities in subsonic and transonic regimes. Readers will see how shock shape choices affect solution regions and the presence of hidden regions, envelopes, and limiting lines.
- Derivation of the governing equations for steady, compressible, inviscid, axially symmetric flow
- Shock conditions, shape selection, and their impact on the solution region
- Comparative methods: characteristic normal form versus a direct three-dimensional numerical approach
- Practical insights into stability criteria, data extension into the complex plane, and handling low Mach number flows
Ideal for readers of advanced fluid dynamics and computational methods who seek a thorough, math‑driven treatment of hypersonic flow problems.
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Computation of Hypersonic Axially Symmetric Flow at Low Mach Numbers
impression à la demandeVendeur : Forgotten Books, London, Royaume-Uni
Évaluation du vendeur 4 sur 5 étoiles
Paperback. Etat : New. Print on Demand. This book explores the flow of compressible fluid around an axially symmetric blunt body in a steady supersonic flow. The author, a mathematician, approaches the problem by solving a Cauchy problem for the equations of motion after first reducing them to characteristic normal form. This allows for the study of the behavior of the flow between the body and shock for low Mach numbers, where the detachment distance is relatively large and singularities in the flow are more likely to appear. The book's significance lies in its contribution to the understanding of the complex interactions between fluid dynamics and geometry in supersonic flows, providing valuable insights for researchers in fluid mechanics, aerodynamics, and related fields. 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 9781333637644_0
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EUR 15,66
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Expédition depuis Royaume-Uni vers Etats-Unis
Expédition depuis Royaume-Uni vers Etats-Unis
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Computation of Hypersonic Axially Symmetric Flow at Low Mach Numbers Classic Reprint
Vendeur : PBShop.store US, Wood Dale, IL, Etats-Unis
Évaluation du vendeur 5 sur 5 étoiles
PAP. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur LW-9781333637644
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EUR 22,27
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Expédition nationale : Etats-Unis
Expédition nationale : Etats-Unis
Quantité disponible : 15 disponible(s)
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Computation of Hypersonic Axially Symmetric Flow at Low Mach Numbers Classic Reprint
Vendeur : PBShop.store UK, Fairford, GLOS, Royaume-Uni
Évaluation du vendeur 5 sur 5 étoiles
PAP. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur LW-9781333637644
Acheter neuf
EUR 24,36
Expédition à EUR 3,81
Expédition depuis Royaume-Uni vers Etats-Unis
Expédition depuis Royaume-Uni vers Etats-Unis
Quantité disponible : 15 disponible(s)