Abstract
Fluid mechanics is not only applicable to aerospace, but also to our mechanical design, considering the comprehensive ability to make our manufacturing more reasonable and accurate, and keep us safe. In this paper, the fluidity of air fluid is analyzed and studied by programming method. By changing different parameters, different flow field distribution diagrams are finally obtained. The research results have reference value for practical engineering applications.
Publisher
Darcy & Roy Press Co. Ltd.
Reference11 articles.
1. S. Takanashi, An iterative procedure for three-dimensional transonic wing design by the integral equation method, 2nd Applied Aerodynamics Conference. 34 (1984) 201-211.
2. W. Bartelheimer, Design of transonic airfoils and wings based on the solution of the Euler/Navier-Stokes equation, Germany, German Aerospace Center, 1994.
3. L. F. Campanile, The belt rib concept f or variable camber airfoil : recent development, Smart Structures and Materials 2000: Smart Structures and Integrated Systems, Proceedings of SPIE. 45 (2000) 110-120.
4. Z. Sun, X. Miao, C. Jagadeesh, Experimental investigation of the transonic shock-wave/boundary-layer interaction over a shock-generation bump, Physics of Fluids. 32 (2022) 106102.
5. P. Wang, M. Zhao, Z. Yan, Dynamic simulation analysis of multi-flexible body of telescopic wing deformation mechanism, Science Technology and Engineering. 9 (2009) 3708-3712.