DocumentCode :
2371405
Title :
Trajectory of a Baseball and Its Characters Under the Influence of a Drag Force and the Magnus Effect
Author :
Sarafian, Haiduke
Author_Institution :
Univ. Coll., Pennsylvania State Univ., York, PA, USA
fYear :
2011
fDate :
20-23 June 2011
Firstpage :
51
Lastpage :
59
Abstract :
A flying baseball in the air not only is subject to gravity´s pull it is also subject to air resistance. A spinning ball in addition to these two forces experiences a spin-dependent force. The description of motion of a baseball subject to these three forces for a projectile confined to trajectories in a 2D vertical plane is a set of two coupled nonlinear ODEs. The speed dependent drag coefficient makes these equations highly nonlinear. These equations for certain cases are solved numerically by applying a 4th-order Runge-Kutta code written in either the FORTRAN or the C++ languages. In this article we show by deploying Mathematica one may easily bypass the explicit need of composing such cumbersome computer codes. Moreover, by utilizing Mathematica´s integrated numeric and graphic features the author reveals features of a flying ball that to-date have not been reported in scientific literature.
Keywords :
C++ language; FORTRAN; Runge-Kutta methods; aerodynamics; drag; gravitation; mathematics computing; physics computing; projectiles; 4rth-order Runge-Kutta code; C++ language; FORTRAN; Magnus effect; Mathematica integrated graphic features; Mathematica integrated numeric features; air resistance; coupled nonlinear ODEs; drag force effect; flying baseball trajectory characteristics; gravity pull; speed dependent drag coefficient; spin-dependent force; spinning ball; Drag; Equations; Force; Frequency modulation; Projectiles; Sports equipment; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational Science and Its Applications (ICCSA), 2011 International Conference on
Conference_Location :
Santander
Print_ISBN :
978-1-4577-0142-9
Type :
conf
DOI :
10.1109/ICCSA.2011.29
Filename :
5959561
Link To Document :
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