A high precision direct integration scheme for flying bodies subjected to transient dynamic loading
  
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DOI:10.7511/jslx19983045
KeyWord:flying bodies,dynamic responsesl/step-by-step integration scheme
Zhang Yahui  Lin Jiahao
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Abstract:
      The dynamic responses of structures with rigid freedoms can not be computed directly by meaans of the published high precision direct integration method. This problem is solved in this paper , so that accurate responses can how be obtained even for very large time-step sizes.