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contributor authorTsai-Chen Soong
date accessioned2017-05-08T22:57:51Z
date available2017-05-08T22:57:51Z
date copyrightJune, 1975
date issued1975
identifier issn0021-8936
identifier otherJAMCAV-26035#257_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/87078
description abstractWolferman of West Germany won the 1972 World Olympic javelin throw with a throw of 296 ft 10 in. (90.47m). Lusis of the USSR came in second with a throw of 1 in. (2.5cm) less. Had he paid a little more attention to technical details, he could have won. In the present paper, five nonlinear, dynamic differential equations which describe a javelin in flight, the wind effect included, are derived, and a numerical solution is proposed. A case study shows that 3.31m (10.9 ft) could be added to the 1972 record by using a throw angle and initial javelin axis angle of 42 and 35 deg, respectively, instead of the conventional angles of 35 deg. Slightly modifying the contour of the javelin profile, legitimate within current NCAA rules, to move the center of the pressure drag forward to 0.8cm behind its center of gravity, instead of the present 25.7cm, gives an additional gain in range of 16.13m (52.9 ft).
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Dynamics of Javelin Throw
typeJournal Paper
journal volume42
journal issue2
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.3423563
journal fristpage257
journal lastpage262
identifier eissn1528-9036
keywordsDynamics (Mechanics)
keywordsCenter of mass
keywordsDifferential equations
keywordsWind
keywordsFlight AND Form drag
treeJournal of Applied Mechanics:;1975:;volume( 042 ):;issue: 002
contenttypeFulltext


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