Using the non-structural dynamic grid technology combined with the spring approximation and the grid reconstruction, the coupling solves the Euler equation and the ballistic equation, and the simulated flight is 46 thousand Meters, 0 ° Angle of attack, Mach number 6.5, shell separation velocity of 6 MPS respectively, 12 MPS, shell separated angular velocity of 0 ° / s respectively, 50 ° / s, 150 ° / s of shrapnel The shell dynamic process. - The use of spring approximation and mesh reconstruction of a combination of non - structural dynamic grid technology, The coupled equations for solving Euler equations and ballistics, flight simulation at 46 km led, 0 ° Angle of attack, Mach 6.5, The shell - chip separation velocity, six MPS respectively, 12 MPS, presents separation of The shell pieces were 0 ° / s, 50 ° / s, 150 ° / s of The cluster bombs thrown shell dynamic process.

子母弹抛壳过程非定常流动的数值模拟.pdf

• We are an exchange download platform that only provides communication channels. The downloaded content comes from the internet. Except for download issues, please Google on your own.
• The downloaded content is provided for members to upload. If it unintentionally infringes on your copyright, please contact us.
• Please use Winrar for decompression tools
• If download fail, Try it againg or Feedback to us.
• If downloaded content did not match the introduction, Feedback to us，Confirm and will be refund.
• Before downloading, you can inquire through the uploaded person information

Nothing．