Applied Mathematics and Mechanics (English Edition) ›› 1994, Vol. 15 ›› Issue (11): 1087-1091.

• 论文 • 上一篇    

THE DIFFERENTIAL SOLUTION TO THE FLYING LOCUS EQUATION OF THE SHOT AND ITS APPLICATION

刘小湘   

  1. Xiangtan instituie of Machinery and Electricity, Technology, Xiangtan
  • 收稿日期:1993-06-19 出版日期:1994-11-18 发布日期:1994-11-18

THE DIFFERENTIAL SOLUTION TO THE FLYING LOCUS EQUATION OF THE SHOT AND ITS APPLICATION

Liu Xiao-xiang   

  1. Xiangtan instituie of Machinery and Electricity, Technology, Xiangtan
  • Received:1993-06-19 Online:1994-11-18 Published:1994-11-18

摘要: This paper establishes a locus equation of the shot according to kinematicalprinciples. By using differential and integral calculus and trigonometric function, wehave found the extreme valve of the angles of delivery and the best flying distances,with the falling poinis of shot considered. Thus a simple expression showing therelationships among the best angle delivery, the best.flying distance, the height ofdelivery point and its initial velocity. can be attained and a diagram can be made bycalculating, showing the best angle of delivery. and the best flying distance.

关键词: influence line method, analytical method, finite element method, microcirculatory dynamics

Abstract: This paper establishes a locus equation of the shot according to kinematicalprinciples. By using differential and integral calculus and trigonometric function, wehave found the extreme valve of the angles of delivery and the best flying distances,with the falling poinis of shot considered. Thus a simple expression showing therelationships among the best angle delivery, the best.flying distance, the height ofdelivery point and its initial velocity. can be attained and a diagram can be made bycalculating, showing the best angle of delivery. and the best flying distance.

Key words: influence line method, analytical method, finite element method, microcirculatory dynamics

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