Dynamic Simulation of Insulation Material Ablation Process in Solid Propellant Rocket Motor-Reference-Cited by-同舟云学术

Dynamic Simulation of Insulation Material Ablation Process in Solid Propellant Rocket Motor

Published:2015-09 Issue:5 Volume:28 Page:04014118
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Xu Yi Hua¹,Hu Xu²,Yang Yu Xin³,Zeng Zhuo Xiong⁴,Hu Chun Bo⁵

Affiliation:

1. Doctor of Technical Science, School of Aircraft Engineering, Nanchang Hangkong Univ., Nanchang, Jiangxi 330063, China (corresponding author).

2. M.S. Candidate, School of Aircraft Engineering, Nanchang Hangkong Univ., Nanchang, Jiangxi 330063, China.

3. Associate Research Fellow, Xi’an Institute of Aerospace Power Technology, Xi’an, Shaanxi 710025, China.

4. Professor, School of Aircraft Engineering, Nanchang Hangkong Univ., Nanchang, Jiangxi 330063, China.

5. Professor, Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000452

Reference44 articles.

1. Bizot A. (1995). “Turbulent boundary layer with mass transfer and pressure gradient in solid propellant rocket motors.” AIAA Paper 95-2708 AIAA Reston VA.

2. Modeling of graphite oxidation in a stagnation-point flow field using detailed homogeneous and semiglobal heterogeneous mechanisms with comparisons to experiments

3. Mars Pathfinder trajectory based heating and ablation calculations

4. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis

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