Large-Eddy Simulation of Supersonic Capsule-Rigid Disk-Gap-Band Parachute Systems

GONG Sheng; WU Chuijie

doi:10.21656/1000-0887.410274

Volume 42 Issue 3

Mar. 2021

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GONG Sheng, WU Chuijie. Large-Eddy Simulation of Supersonic Capsule-Rigid Disk-Gap-Band Parachute Systems[J]. Applied Mathematics and Mechanics, 2021, 42(3): 233-247. doi: 10.21656/1000-0887.410274

Citation:

GONG Sheng, WU Chuijie. Large-Eddy Simulation of Supersonic Capsule-Rigid Disk-Gap-Band Parachute Systems[J]. Applied Mathematics and Mechanics, 2021, 42(3): 233-247. doi: 10.21656/1000-0887.410274

Citation:

GONG Sheng, WU Chuijie. Large-Eddy Simulation of Supersonic Capsule-Rigid Disk-Gap-Band Parachute Systems[J]. Applied Mathematics and Mechanics, 2021, 42(3): 233-247. doi: 10.21656/1000-0887.410274

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Large-Eddy Simulation of Supersonic Capsule-Rigid Disk-Gap-Band Parachute Systems

doi: 10.21656/1000-0887.410274

School of Aeronautics and Astronautics, Dalian University of Technology,Dalian, Liaoning 116024, P.R.China

Funds: The National Natural Science Foundation of China（11372068）

Received Date: 2020-09-14
Rev Recd Date: 2020-09-28
Publish Date: 2021-03-01

Abstract

Abstract

The influences of the aerodynamic deceleration performance and the flow field structure characteristics of the capsule-rigid disk-gap-band parachute system at an initial Mach number of 2.0 and different block-structured adaptive mesh refinement were studied. In the unsteady compressible fluid, the hybrid WENO (weighted essentially non-oscillatory) and TCD (tuned center difference) schemes were used to simulate the shock wave and the smooth continuous flow field. The large-eddy simulation method with the stretched vortex subgrid model was used to deal with the turbulence. The results show that, at a low resolution of the block-structured adaptive mesh refinement, it is difficult to accurately simulate the important aerodynamic drag coefficient and capture the flow field characteristics of the parachute system. Subsequently, the convergence of the adaptive mesh refinement of the flow field was verified.
- adaptive mesh refinement,
- large-eddy simulation,
- supersonic flow,
- disk-gap-band parachute

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References(20)

References

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