Bin Wang1, Jing Zheng1, Yuanyuan Yu1,2, Runmin Lv1, Changyue Xu1,*
FDMP-Fluid Dynamics & Materials Processing, Vol.16, No.4, pp. 675-684, 2020, DOI:10.32604/fdmp.2020.09681
- 11 August 2020
Abstract Rocket sleds belong to a category of large-scale test platforms running
on the ground. The applications can be found in many fields, such as aerospace
engineering, conventional weapons, and civil high-tech products. In the present
work, shock-wave/rail-fasteners interaction is investigated numerically when the
rocket sled is in supersonic flow conditions. Two typical rocket sled models are
considered, i.e., an anti-D shaped version of the rocket sled and an axisymmetric
slender-body variant. The dynamics for Mach number 2 have been simulated in
the framework of a dynamic mesh method. The emerging shock waves can be
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