Optimization of the aerodynamic configuration of a tubular projectile based on blind kriging

Document Type : Article

Authors

National Key Laboratory of Transient Physics, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China

Abstract

Based on optimal Latin hypercube design for computer experiments, blind Kriging surrogate model and sequential quadratic programming method, the optimal design of the aerodynamic configuration of a 30mm tubular projectile is carried out with the use of commercial softwares, such as UG, ICEM CFD, FLUENT etc. The aerodynamic configuration has been optimized to minimize the drag coefficients at different Mach numbers and maximize the kinetic energies at given flight ranges. The optimal configuration is obtained and discussed. Finally, the similarities and differences of the flow structure and aerodynamic characteristics between the original and optimal tubular projectiles are compared. The numerical optimal method proposed in this paper for optimizing the tubular projectile can provide important guidances for the aerodynamic configuration design of projectiles.

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Main Subjects


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Volume 26, Issue 1
Transactions on Mechanical Engineering (B)
January and February 2019
Pages 311-322
  • Receive Date: 07 December 2016
  • Revise Date: 02 August 2017
  • Accept Date: 25 December 2017