Application of immersed boundary method to the simulation of transient flow in solid rocket motors-Reference-Cited by-同舟云学术

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Application of immersed boundary method to the simulation of transient flow in solid rocket motors

Published:2021-12 Issue: Volume:119 Page:107228
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Lin Qingyu,Jiang Kun^ORCID,Wang Hao,Wang Jinlong

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference54 articles.

1. Coupled simulation of fluid flow and propellant burning surface regression in a solid rocket motor;Li;Comput. Fluids,2014

2. Accurate computation of grain burning coupled with flow simulation in rocket chamber;Gueyffier;J. Propuls. Power,2015

3. Applications of dynamic hybrid grid method for three-dimensional moving/deforming boundary problems;Zhang;Comput. Fluids,2012

4. Unsteady Euler algorithm with unstructured dynamic mesh for complex-aircraft aerodynamic analysis;Batina;AIAA J.,1991

5. Considerations on the spring analogy;Blom;Int. J. Numer. Methods Fluids,2000

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Simulation of Gas Flow Coupled with Burning Surface Regression Based on Immersed Boundary Method and Face Offsetting Method;Aerospace;2024-07-04

2. Numerical study of the impact and aggregation characteristics of alumina droplets on a wall in the solid rocket motor;Aerospace Science and Technology;2023-06

3. Application of immersed boundary method to the simulation of three-dimensional flow in solid rocket motors;AIP Advances;2023-06-01

4. Development of Wall Injection Model for Solid Rocket Motor Internal Flow by Block-Structure Cartesian Mesh;AIAA SCITECH 2023 Forum;2023-01-19

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