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Numerical Computation of Hypersonic Flow Past a Two-dimensional Blunt Body

About Numerical Computation of Hypersonic Flow Past a Two-dimensional Blunt Body

This book provides a comprehensive guide to the numerical computation of hypersonic flow past a two-dimensional blunt body. The author presents the mathematical and computational techniques required for accurate simulation and analysis of hypersonic flow, as well as practical considerations and examples of their application. This book is a valuable resource for researchers, engineers, and students working in the areas of hypersonic aerodynamics and computational fluid dynamics. 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 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. 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.

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  • Language:
  • English
  • ISBN:
  • 9781019527849
  • Binding:
  • Hardback
  • Published:
  • July 17, 2023
  • Dimensions:
  • 156x234x6 mm.
  • Weight:
  • 286 g.
Delivery: 2-3 weeks
Expected delivery: December 19, 2024
Extended return policy to January 30, 2025

Description of Numerical Computation of Hypersonic Flow Past a Two-dimensional Blunt Body

This book provides a comprehensive guide to the numerical computation of hypersonic flow past a two-dimensional blunt body. The author presents the mathematical and computational techniques required for accurate simulation and analysis of hypersonic flow, as well as practical considerations and examples of their application. This book is a valuable resource for researchers, engineers, and students working in the areas of hypersonic aerodynamics and computational fluid dynamics.
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 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.
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.

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