國立高雄大學圖資館 |

登入

回首頁

Wing theoryincompressible fluids /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Wing theoryby Gil Iosilevskii.
其他題名:	incompressible fluids /
作者:	Iosilevskii, Gil.
出版者:	Cham :Springer Nature Switzerland :2025.
面頁冊數:	x, 265 p. :ill. (some col.), digital ;24 cm.
Contained By:	Springer Nature eBook
標題:	AirplanesWings.
電子資源:	https://doi.org/10.1007/978-3-031-73625-4
ISBN:	9783031736254$q(electronic bk.)

Wing theoryincompressible 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$q(electronic bk.)

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

769135
Airplanes
--Wings.

LC Class. No.: TL672

Dewey Class. No.: 629.13432

Wing theoryincompressible fluids /
LDR:02246nmm a2200325 a 4500 001 678182
003 DE-He213
005 20250410135742.0
006 m d
007 cr nn 008maaau
008 251021s2025 sz s 0 eng d
020 $a 9783031736254$q(electronic bk.)
020 $a 9783031736247$q(paper)
024 7 $a 10.1007/978-3-031-73625-4 $2 doi
035 $a 978-3-031-73625-4
040 $a GP $c GP
041 0 $a eng
050 4 $a TL672
072 7 $a TGMF $2 bicssc
072 7 $a TEC009070 $2 bisacsh
072 7 $a TGMF $2 thema
082 0 4 $a 629.13432 $2 23
090 $a TL672 $b .I64 2025
100 1 $a Iosilevskii, Gil. $3 991610
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 769135
650 0 $a Aerodynamics. $3 216234
650 1 4 $a Engineering Fluid Dynamics. $3 273893
650 2 4 $a Aerospace Technology and Astronautics. $3 309707
650 2 4 $a Classical and Continuum Physics. $3 771188
710 2 $a SpringerLink (Online service) $3 273601
773 0 $t Springer Nature eBook
856 4 0 $u https://doi.org/10.1007/978-3-031-73625-4
950 $a Physics and Astronomy (SpringerNature-11651)