Volume 25 Issue 1
Jan.  2010
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LI Jian-ping, BAI Chun-hua. Analysis of flight stability and rear flow field of the cargo projectile[J]. Journal of Aerospace Power, 2010, 25(1): 107-113.
Citation: LI Jian-ping, BAI Chun-hua. Analysis of flight stability and rear flow field of the cargo projectile[J]. Journal of Aerospace Power, 2010, 25(1): 107-113.

Analysis of flight stability and rear flow field of the cargo projectile

  • Received Date: 2008-12-16
  • Rev Recd Date: 2009-05-04
  • Publish Date: 2010-01-28
  • Flight stability and rear flow fields of the cargo projectile were studied by simulation test and numerical computation.The cargo projectile can fly stably and the results of simulation test agree well with numerical computation.In addition,the rear pressure distribution was also obtained by numerical computation,showing that there are eddy-current zones at the bomb rear,which will increase with the flight speed.

     

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      沈阳化工大学材料科学与工程学院 沈阳 110142

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