Fundamentals of Modern Unsteady Aerodynamics
Autor Ülgen Gülçaten Limba Engleză Hardback – 5 ian 2021
This 3rd edition includes a new chapter about unsteady applications related to the thrust optimization, aerodynamic stability and trim because there has been much progress in unsteady applications of the flapping wing technology. In addition, further material is presented in Appendix for evaluating the stability derivatives so that no derivation of equations is left incomplete but not overdone in the text.
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Specificații
ISBN-13: 9783030607760
ISBN-10: 3030607763
Ilustrații: XVI, 435 p. 219 illus., 8 illus. in color.
Dimensiuni: 155 x 235 mm
Greutate: 0.81 kg
Ediția:3rd ed. 2021
Editura: Springer International Publishing
Colecția Springer
Locul publicării:Cham, Switzerland
ISBN-10: 3030607763
Ilustrații: XVI, 435 p. 219 illus., 8 illus. in color.
Dimensiuni: 155 x 235 mm
Greutate: 0.81 kg
Ediția:3rd ed. 2021
Editura: Springer International Publishing
Colecția Springer
Locul publicării:Cham, Switzerland
Cuprins
Introduction.- Fundamental Equations.- Incompressible Flow About an Airfoil.- Incompressible Flow About Thin Wings.- Subsonic and Supersonic Flows.- Transonic flow.- Hypersonic Flow.- Modern Subjects.- Unsteady Applications related to the thrust optimization, aerodynamic stability and trim.- Aerodynamics: The Outlook for the Future.
Notă biografică
Dr. Ülgen GÜLÇAT is Emeritus Professor at the Faculty of Aeronautics and Astronautics of Istanbul Technical University (ITU).
He is expert in Computational Fluid Dynamics and studies the interaction of fluids with airfoils.
Textul de pe ultima copertă
This book introduces the concept of unsteady aerodynamics and its underlying principles. The author provides the readers with a comprehensive review of the fundamental physics of free and forced unsteadiness, the terminology and basic equations of aerodynamics ranging from incompressible flow to hypersonics. The book also covers modern topics related to the developments made in recent years, especially in relation to wing flapping for propulsion. The book is written for graduate and senior year undergraduate students in aerodynamics and also serves as a reference for experienced researchers. Each chapter includes ample examples, questions, problems and relevant references.
This 3rd edition includes a new chapter about unsteady applications related to the thrust optimization, aerodynamic stability and trim because there has been much progress in unsteady applications of the flapping wing technology. In addition, further material is presented in Appendix for evaluating thestability derivatives so that no derivation of equations is left incomplete but not overdone in the text.
This 3rd edition includes a new chapter about unsteady applications related to the thrust optimization, aerodynamic stability and trim because there has been much progress in unsteady applications of the flapping wing technology. In addition, further material is presented in Appendix for evaluating thestability derivatives so that no derivation of equations is left incomplete but not overdone in the text.
Caracteristici
Provides a clear introduction to the fundamental physics and basic equations of aerodynamics Covers modern topics related to developments in recent years Offers much more insight to thrust optimization and aerodynamic stability
Recenzii
From the reviews:
“This monograph, giving the progress in unsteady aerodynamics during about a century, is written as a graduate textbook. An additional aim is to provide the practicing engineers with the knowledge of the most recent developments in unsteady aerodynamics. … the author presents a three-dimensional analysis of swept wings with extra lift created by leading edge separation. Ten appendices supplement the formulae used in the basic text.” (Boris V. Loginov, Zentralblatt MATH, Vol. 1216, 2011)
“This monograph, giving the progress in unsteady aerodynamics during about a century, is written as a graduate textbook. An additional aim is to provide the practicing engineers with the knowledge of the most recent developments in unsteady aerodynamics. … the author presents a three-dimensional analysis of swept wings with extra lift created by leading edge separation. Ten appendices supplement the formulae used in the basic text.” (Boris V. Loginov, Zentralblatt MATH, Vol. 1216, 2011)