@inbook{c5ad9865cd3d4c33b92ead14d0a37c6f,
title = "Notice of Retraction: Optimization design of the rocket launching facilities and the thermal protection",
abstract = "Based on fully hexahedral mesh and the k-e turbulence model, the computational fluid dynamics method was used to the numerical simulation. Different angle of the double-faced deflector and the thermal protection of the launching facilities were calculated. The pressure and temperature parameters were obtained and the result was compared and analyzed. The appropriate model was selected. The numerical calculation method and the results can be used to the engineering.",
keywords = "Deflector, Launching facilities, Rocket plume, Simulation, Thermal protection",
author = "Yi Jiang and Ma, {Yan Li} and Wang, {Wei Chen} and Hao, {Ji Guang}",
year = "2010",
doi = "10.1109/ICACC.2010.5487017",
language = "English",
isbn = "9781424458462",
series = "Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010",
publisher = "IEEE Computer Society",
pages = "30--33",
booktitle = "Proceedings - 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010",
address = "United States",
}