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Wing theory = incompressible fluids /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Wing theory/ by Gil Iosilevskii.
Reminder of title:	incompressible fluids /
Author:	Iosilevskii, Gil.
Published:	Cham :Springer Nature Switzerland : : 2025.,
Description:	x, 265 p. :ill. (some col.), digital ;24 cm.
[NT 15003449]:	1.Introduction -- 2.Thick wing sections in steady motion -- 3.Thin wing sections in steady motion -- 4.Thin wing sections in non-uniform motion -- 5.Permeable membrane wings -- 6.Partially separated wake -- 7.Linearized theory of thin wings of finite span -- 8.High-aspect-ratio wings in steady motion -- 9.High-aspect-ratio wings in nonuniform motion -- 10.Drag, losses and the Trefftz plane -- 11.Low-aspect-ratio wings in nonuniform motion.
Contained By:	Springer Nature eBook
Subject:	Airplanes - Wings. -
Online resource:	https://doi.org/10.1007/978-3-031-73625-4
ISBN:	9783031736254

Wing theory = incompressible fluids /
Iosilevskii, Gil.

Wing theoryincompressible fluids /[electronic resource] :by Gil Iosilevskii. - Cham :Springer Nature Switzerland :2025. - x, 265 p. :ill. (some col.), digital ;24 cm.

1.Introduction -- 2.Thick wing sections in steady motion -- 3.Thin wing sections in steady motion -- 4.Thin wing sections in non-uniform motion -- 5.Permeable membrane wings -- 6.Partially separated wake -- 7.Linearized theory of thin wings of finite span -- 8.High-aspect-ratio wings in steady motion -- 9.High-aspect-ratio wings in nonuniform motion -- 10.Drag, losses and the Trefftz plane -- 11.Low-aspect-ratio wings in nonuniform motion.

A high Reynolds number flow about a lifting wing typically forms a thin boundary layer on its surface, which smoothly merges with a thin vortical wake behind it. An asymptotic theory, based on wing's thickness, camber, angle of attack and aspect ratio, can turn this simple observation into a fair approximation for the pressure loads acting on a finite wing in generally non-uniform motion. This book unfolds this theory step-by-step, revisiting a few well-known and some less-known results along the way. The fidelity of the approximation is demonstrated in numerous examples. The stress in the book is on mathematical rigor, and all non-trivial steps are scrutinized in numerous appendices. The book can be a basis for a graduate course on theoretical aerodynamics, but can also be a reference for quite a few practical aerodynamic models.

ISBN: 9783031736254

Standard No.: 10.1007/978-3-031-73625-4doiSubjects--Topical Terms:

3214575
Airplanes
--Wings.

LC Class. No.: TL672

Dewey Class. No.: 629.13432

Wing theory = incompressible fluids /
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100 1 $a Iosilevskii, Gil. $3 3784375
245 1 0 $a Wing theory $h [electronic resource] : $b incompressible fluids / $c by Gil Iosilevskii.
260 $a Cham : $b Springer Nature Switzerland : $b Imprint: Springer, $c 2025.
300 $a x, 265 p. : $b ill. (some col.), digital ; $c 24 cm.
505 0 $a 1.Introduction -- 2.Thick wing sections in steady motion -- 3.Thin wing sections in steady motion -- 4.Thin wing sections in non-uniform motion -- 5.Permeable membrane wings -- 6.Partially separated wake -- 7.Linearized theory of thin wings of finite span -- 8.High-aspect-ratio wings in steady motion -- 9.High-aspect-ratio wings in nonuniform motion -- 10.Drag, losses and the Trefftz plane -- 11.Low-aspect-ratio wings in nonuniform motion.
520 $a A high Reynolds number flow about a lifting wing typically forms a thin boundary layer on its surface, which smoothly merges with a thin vortical wake behind it. An asymptotic theory, based on wing's thickness, camber, angle of attack and aspect ratio, can turn this simple observation into a fair approximation for the pressure loads acting on a finite wing in generally non-uniform motion. This book unfolds this theory step-by-step, revisiting a few well-known and some less-known results along the way. The fidelity of the approximation is demonstrated in numerous examples. The stress in the book is on mathematical rigor, and all non-trivial steps are scrutinized in numerous appendices. The book can be a basis for a graduate course on theoretical aerodynamics, but can also be a reference for quite a few practical aerodynamic models.
650 0 $a Airplanes $x Wings. $3 3214575
650 0 $a Aerodynamics. $3 532569
650 1 4 $a Engineering Fluid Dynamics. $3 891349
650 2 4 $a Aerospace Technology and Astronautics. $3 928116
650 2 4 $a Classical and Continuum Physics. $3 3218450
710 2 $a SpringerLink (Online service) $3 836513
773 0 $t Springer Nature eBook
856 4 0 $u https://doi.org/10.1007/978-3-031-73625-4
950 $a Physics and Astronomy (SpringerNature-11651)