Elements of Vorticity Aerodynamics (Record no. 77289)
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000 -LEADER | |
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fixed length control field | 03812nam a22006015i 4500 |
001 - CONTROL NUMBER | |
control field | 978-3-662-44040-7 |
005 - DATE AND TIME OF LATEST TRANSACTION | |
control field | 20220801215245.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
fixed length control field | 171228s2018 gw | s |||| 0|eng d |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
ISBN | 9783662440407 |
-- | 978-3-662-44040-7 |
082 04 - CLASSIFICATION NUMBER | |
Call Number | 620.3 |
100 1# - AUTHOR NAME | |
Author | Wu, James C. |
245 10 - TITLE STATEMENT | |
Title | Elements of Vorticity Aerodynamics |
250 ## - EDITION STATEMENT | |
Edition statement | 1st ed. 2018. |
300 ## - PHYSICAL DESCRIPTION | |
Number of Pages | X, 140 p. 2 illus., 1 illus. in color. |
490 1# - SERIES STATEMENT | |
Series statement | Springer Tracts in Mechanical Engineering, |
505 0# - FORMATTED CONTENTS NOTE | |
Remark 2 | Introduction -- Theorems of Helmholtz and Kelvin -- Vorticity Kinematics -- Vorticity Kinetics -- Vorticity-Moment Theorem -- Classical Aerodynamics -- Unsteady Aerodynamics. |
520 ## - SUMMARY, ETC. | |
Summary, etc | This book opens with a discussion of the vorticity-dynamic formulation of the low Mach number viscous flow problem. It examines the physical aspects of the velocity and the vorticity fields, their instantaneous relationship, and the transport of vorticity in viscous fluids for steady and unsteady flows. Subsequently, using classical analyses it explores the mathematical aspects of vorticity dynamics and issues of initial and boundary conditions for the viscous flow problem. It also includes the evolution of the vorticity field which surrounds and trails behind airfoils and wings, generalizations of Helmholtz’ vortex theorems and the Biot-Savart Law. The book introduces a theorem that relates the aerodynamic force to the vorticity moment and reviews the applications of the theorem. Further, it presents interpretations of the Kutta-Joukowski theorem and Prandtl’s lifting line theory for vorticity dynamics and discusses wake integral methods. The virtual-mass effect is shown to be the seminal event in unsteady aerodynamics and a simple approach for evaluating virtual-mass forces on the basis of vorticity dynamics is presented. The book presents a modern viewpoint on vorticity dynamics as the framework for understanding and establishing the fundamental principles of viscous and unsteady aerodynamics. It is intended for graduate-level students of classical aerodynamics and researchers exploring the frontiers of fully unsteady and non-streamlined aerodynamics. |
856 40 - ELECTRONIC LOCATION AND ACCESS | |
Uniform Resource Identifier | https://doi.org/10.1007/978-3-662-44040-7 |
942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
Koha item type | eBooks |
264 #1 - | |
-- | Berlin, Heidelberg : |
-- | Springer Berlin Heidelberg : |
-- | Imprint: Springer, |
-- | 2018. |
336 ## - | |
-- | text |
-- | txt |
-- | rdacontent |
337 ## - | |
-- | computer |
-- | c |
-- | rdamedia |
338 ## - | |
-- | online resource |
-- | cr |
-- | rdacarrier |
347 ## - | |
-- | text file |
-- | |
-- | rda |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Multibody systems. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Vibration. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Mechanics, Applied. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Continuum mechanics. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Fluid mechanics. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Aerospace engineering. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Astronautics. |
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Multibody Systems and Mechanical Vibrations. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Continuum Mechanics. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Engineering Fluid Dynamics. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Aerospace Technology and Astronautics. |
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
-- | 2195-9870 |
912 ## - | |
-- | ZDB-2-ENG |
912 ## - | |
-- | ZDB-2-SXE |
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