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Introduction to transonic aerodynamics
~
Vos, Roelof.
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Introduction to transonic aerodynamics
Record Type:
Electronic resources : Monograph/item
Title/Author:
Introduction to transonic aerodynamics/ by Roelof Vos, Saeed Farokhi.
Author:
Vos, Roelof.
other author:
Farokhi, Saeed.
Published:
Dordrecht :Springer Netherlands : : 2015.,
Description:
xiii, 555 p. :ill., digital ;24 cm.
[NT 15003449]:
1 Introduction and Historic Perspective -- 2 Review of Fundamental Equations -- 3 Transonic Similarity Laws -- 4 Shock-Expansion Theory -- 5 Method of Characteristics -- 6 Aerodynamics of Non lifting Bodies -- 7 Airfoil Aerodynamics -- 8 Aerodynamics of Swept Wings -- A Isentropic Flow Table -- B Normal Shock Table -- C Prandtl-Meyer Function -- Partial Answers to Selected Problems -- Glossary -- Index.
Contained By:
Springer eBooks
Subject:
Aerodynamics, Transonic. -
Online resource:
http://dx.doi.org/10.1007/978-94-017-9747-4
ISBN:
9789401797474 (electronic bk.)
Introduction to transonic aerodynamics
Vos, Roelof.
Introduction to transonic aerodynamics
[electronic resource] /by Roelof Vos, Saeed Farokhi. - Dordrecht :Springer Netherlands :2015. - xiii, 555 p. :ill., digital ;24 cm. - Fluid mechanics and its applications,v.1100926-5112 ;. - Fluid mechanics and its applications ;v.98..
1 Introduction and Historic Perspective -- 2 Review of Fundamental Equations -- 3 Transonic Similarity Laws -- 4 Shock-Expansion Theory -- 5 Method of Characteristics -- 6 Aerodynamics of Non lifting Bodies -- 7 Airfoil Aerodynamics -- 8 Aerodynamics of Swept Wings -- A Isentropic Flow Table -- B Normal Shock Table -- C Prandtl-Meyer Function -- Partial Answers to Selected Problems -- Glossary -- Index.
Written to teach students the nature of transonic flow and its mathematical foundation, this book offers a much-needed introduction to transonic aerodynamics. The authors present a quantitative and qualitative assessment of subsonic, supersonic, and transonic flow around bodies in two and three dimensions. The book reviews the governing equations and explores their applications and limitations as employed in modeling and computational fluid dynamics. Some concepts, such as shock and expansion theory, are examined from a numerical perspective. Others, including shock-boundary-layer interaction, are discussed from a qualitative point of view. The book includes 60 examples and more than 200 practice problems. The authors also offer analytical methods such as Method of Characteristics (MOC) that allow readers to practice with the subject matter. The result is a wealth of insight into transonic flow phenomena and their impact on aircraft design, including compressibility effects, shock and expansion waves, shock-boundary-layer interaction and aeroelasticity.
ISBN: 9789401797474 (electronic bk.)
Standard No.: 10.1007/978-94-017-9747-4doiSubjects--Topical Terms:
707322
Aerodynamics, Transonic.
LC Class. No.: TL571
Dewey Class. No.: 629.132304
Introduction to transonic aerodynamics
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1 Introduction and Historic Perspective -- 2 Review of Fundamental Equations -- 3 Transonic Similarity Laws -- 4 Shock-Expansion Theory -- 5 Method of Characteristics -- 6 Aerodynamics of Non lifting Bodies -- 7 Airfoil Aerodynamics -- 8 Aerodynamics of Swept Wings -- A Isentropic Flow Table -- B Normal Shock Table -- C Prandtl-Meyer Function -- Partial Answers to Selected Problems -- Glossary -- Index.
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Written to teach students the nature of transonic flow and its mathematical foundation, this book offers a much-needed introduction to transonic aerodynamics. The authors present a quantitative and qualitative assessment of subsonic, supersonic, and transonic flow around bodies in two and three dimensions. The book reviews the governing equations and explores their applications and limitations as employed in modeling and computational fluid dynamics. Some concepts, such as shock and expansion theory, are examined from a numerical perspective. Others, including shock-boundary-layer interaction, are discussed from a qualitative point of view. The book includes 60 examples and more than 200 practice problems. The authors also offer analytical methods such as Method of Characteristics (MOC) that allow readers to practice with the subject matter. The result is a wealth of insight into transonic flow phenomena and their impact on aircraft design, including compressibility effects, shock and expansion waves, shock-boundary-layer interaction and aeroelasticity.
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EB TL571 .V959 2015
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