@inproceedings{cf16ffb8982445e5b7f4d5fc9180865b,
title = "Study on the impact of missile flight mach to its engine thrust",
abstract = "Rocket engine thrust is the main performance parameters. The flow field of missile fight in different Mach is simulated by using FLUENT, then calculating the thrust of different conditions. The calculating results are consistent with the theory of Mach almost no effect on the thrust.",
author = "Liu, {Rui Qing} and Yi Jiang",
note = "Publisher Copyright: {\textcopyright} (2014) Trans Tech Publications, Switzerland.; 2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014 ; Conference date: 30-07-2014 Through 31-07-2014",
year = "2014",
doi = "10.4028/www.scientific.net/AMR.1030-1032.1331",
language = "English",
series = "Advanced Materials Research",
publisher = "Trans Tech Publications Ltd.",
pages = "1331--1336",
editor = "Kao, {Jimmy C.M.} and Wen-Pei Sung and Ran Chen",
booktitle = "Materials, Transportation and Environmental Engineering II",
address = "Switzerland",
}