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Fundamentals of modern unsteady aero...

Gulcat, Ulgen.

Fundamentals of modern unsteady aerodynamics

Record Type:	Electronic resources : Monograph/item
Title/Author:	Fundamentals of modern unsteady aerodynamicsby Ulgen Gulcat.
Author:	Gulcat, Ulgen.
Published:	Cham :Springer International Publishing :2021.
Description:	xvi, 435 p. :ill. (some col.), digital ;24 cm.
Contained By:	Springer Nature eBook
Subject:	Unsteady flow (Aerodynamics)
Online resource:	https://doi.org/10.1007/978-3-030-60777-7
ISBN:	9783030607777$q(electronic bk.)

Fundamentals of modern unsteady aerodynamics
Gulcat, Ulgen.

Fundamentals of modern unsteady aerodynamics[electronic resource] /by Ulgen Gulcat. - Third edition. - Cham :Springer International Publishing :2021. - xvi, 435 p. :ill. (some col.), digital ;24 cm.

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.

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 the stability derivatives so that no derivation of equations is left incomplete but not overdone in the text.

ISBN: 9783030607777$q(electronic bk.)

Standard No.: 10.1007/978-3-030-60777-7doiSubjects--Topical Terms:

493801
Unsteady flow (Aerodynamics)

LC Class. No.: TL574.U5 / G853 2021

Dewey Class. No.: 629.1323

Fundamentals of modern unsteady aerodynamics
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100 1 $a Gulcat, Ulgen. $3 493800
245 1 0 $a Fundamentals of modern unsteady aerodynamics $h [electronic resource] / $c by Ulgen Gulcat.
250 $a Third edition.
260 $a Cham : $b Springer International Publishing : $b Imprint: Springer, $c 2021.
300 $a xvi, 435 p. : $b ill. (some col.), digital ; $c 24 cm.
505 0 $a 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.
520 $a 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 the stability derivatives so that no derivation of equations is left incomplete but not overdone in the text.
650 0 $a Unsteady flow (Aerodynamics) $3 493801
650 0 $a Fluid mechanics. $3 189003
650 0 $a Field theory (Physics) $3 208085
650 0 $a Materials science. $3 221779
650 0 $a Aerospace engineering. $3 324294
650 0 $a Astronautics. $3 274036
650 1 4 $a Engineering Fluid Dynamics. $3 273893
650 2 4 $a Classical and Continuum Physics. $3 771188
650 2 4 $a Materials Science, general. $3 308687
650 2 4 $a Aerospace Technology and Astronautics. $3 309707
710 2 $a SpringerLink (Online service) $3 273601
773 0 $t Springer Nature eBook
856 4 0 $u https://doi.org/10.1007/978-3-030-60777-7
950 $a Physics and Astronomy (SpringerNature-11651)