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Development of a hybrid method in a 3-D numerical burn-back analysis for solid propellant grains

  • Published:2020-11 Issue: Volume:106 Page:106103
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Oh Seok-Hwan,Lee Hyoung Jin,Roh Tae-Seong

Funder

National Research Foundation of Korea

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. Development of three-dimensional numerical model for combustion-flow in interior ballistics;Jang;J. Mech. Sci. Technol.,2016

2. Prediction of Pyroshock-reduced separation nut behaviors;Woo;J. Propuls. Power,2018

3. Modeling of combustion and ignition of solid-propellant ingredients;Beckstead;Prog. Energy Combust. Sci.,2007

4. SRM internal ballistic numerical simulation by SPINBALL model;Cavallini,2009

5. Numerical Burnback Analysis of Three Dimensional Solid Propellant Grains;Ata,2015
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