國立虎尾科技大學 |

Theoretical and Applied Aerodynamics = and Related Numerical Methods /

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Theoretical and Applied Aerodynamics/ by J. J. Chattot, M. M. Hafez.
其他題名:	and Related Numerical Methods /
作者:	Chattot, J. J.
其他作者:	Hafez, M. M.
面頁冊數:	XXI, 620 p. 325 illus., 141 illus. in color.online resource. :
Contained By:	Springer Nature eBook
標題:	Fluids. -
電子資源:	https://doi.org/10.1007/978-94-017-9825-9
ISBN:	9789401798259

Theoretical and Applied Aerodynamics = and Related Numerical Methods /
Chattot, J. J.

Theoretical and Applied Aerodynamicsand Related Numerical Methods /[electronic resource] :by J. J. Chattot, M. M. Hafez. - 1st ed. 2015. - XXI, 620 p. 325 illus., 141 illus. in color.online resource.

Part I Fundamental Aerodynamics -- Introduction -- Inviscid, Incompressible Flow Past Circular Cylinders and Joukowski Airfoils -- Inviscid, Incompressible Flow Past Thin Airfoils -- Inviscid, Compressible Flow Past Thin Airfoils -- Inviscid, Unsteady Flows past Airfoils -- Flow Past Large and Moderate Aspect Ratio Wings -- Axisymmetric Flows and Slender Body Theories -- Viscous Fluid Flow and Laminar Boundary Layers -- Viscous/Inviscid Interaction Procedures -- Part II Special Topics -- Wind Turbine and Propeller Aerodynamics – Analysis and Design -- Glider and Airplane Design -- Introduction to Hypersonic Flows -- Flow Analogies -- Part III Problems and Solutions -- Problems -- Solutions to Problems Appendix: Special Techniques.

This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including: -The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings. - The linearized theories for compressible subsonic and supersonic aerodynamics. - The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained. - Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations. There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows. A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics, and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.

ISBN: 9789401798259

Standard No.: 10.1007/978-94-017-9825-9doiSubjects--Topical Terms:

671110
Fluids.

LC Class. No.: QC138-168.86

Dewey Class. No.: 532

Theoretical and Applied Aerodynamics = and Related Numerical Methods /
LDR:03623nam a22004215i 4500 001 966900
003 DE-He213
005 20200704020331.0
007 cr nn 008mamaa
008 201211s2015 ne | s |||| 0|eng d
020 $a 9789401798259 $9 978-94-017-9825-9
024 7 $a 10.1007/978-94-017-9825-9 $2 doi
035 $a 978-94-017-9825-9
050 4 $a QC138-168.86
050 4 $a QA930
072 7 $a PHDF $2 bicssc
072 7 $a SCI085000 $2 bisacsh
072 7 $a PHDF $2 thema
082 0 4 $a 532 $2 23
082 0 4 $a 533.62 $2 23
100 1 $a Chattot, J. J. $e author. $4 aut $4 http://id.loc.gov/vocabulary/relators/aut $3 1262540
245 1 0 $a Theoretical and Applied Aerodynamics $h [electronic resource] : $b and Related Numerical Methods / $c by J. J. Chattot, M. M. Hafez.
250 $a 1st ed. 2015.
264 1 $a Dordrecht : $b Springer Netherlands : $b Imprint: Springer, $c 2015.
300 $a XXI, 620 p. 325 illus., 141 illus. in color. $b online resource.
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
347 $a text file $b PDF $2 rda
505 0 $a Part I Fundamental Aerodynamics -- Introduction -- Inviscid, Incompressible Flow Past Circular Cylinders and Joukowski Airfoils -- Inviscid, Incompressible Flow Past Thin Airfoils -- Inviscid, Compressible Flow Past Thin Airfoils -- Inviscid, Unsteady Flows past Airfoils -- Flow Past Large and Moderate Aspect Ratio Wings -- Axisymmetric Flows and Slender Body Theories -- Viscous Fluid Flow and Laminar Boundary Layers -- Viscous/Inviscid Interaction Procedures -- Part II Special Topics -- Wind Turbine and Propeller Aerodynamics – Analysis and Design -- Glider and Airplane Design -- Introduction to Hypersonic Flows -- Flow Analogies -- Part III Problems and Solutions -- Problems -- Solutions to Problems Appendix: Special Techniques.
520 $a This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including: -The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings. - The linearized theories for compressible subsonic and supersonic aerodynamics. - The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained. - Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations. There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows. A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics, and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.
650 0 $a Fluids. $3 671110
650 0 $a Fluid mechanics. $3 555551
650 0 $a Physics. $3 564049
650 0 $a Mechanics. $3 527684
650 0 $a Mechanics, Applied. $3 596630
650 0 $a Applied mathematics. $3 1069907
650 0 $a Engineering mathematics. $3 562757
650 1 4 $a Fluid- and Aerodynamics. $3 768779
650 2 4 $a Engineering Fluid Dynamics. $3 670525
650 2 4 $a Numerical and Computational Physics, Simulation. $3 1112293
650 2 4 $a Solid Mechanics. $3 1211586
650 2 4 $a Mathematical and Computational Engineering. $3 1139415
700 1 $a Hafez, M. M. $4 aut $4 http://id.loc.gov/vocabulary/relators/aut $3 857066
710 2 $a SpringerLink (Online service) $3 593884
773 0 $t Springer Nature eBook
776 0 8 $i Printed edition: $z 9789401798242
776 0 8 $i Printed edition: $z 9789401798266
776 0 8 $i Printed edition: $z 9789401777933
856 4 0 $u https://doi.org/10.1007/978-94-017-9825-9
912 $a ZDB-2-PHA
912 $a ZDB-2-SXP
950 $a Physics and Astronomy (SpringerNature-11651)
950 $a Physics and Astronomy (R0) (SpringerNature-43715)