Study on the Impact of Missile Flight Mach to its Engine Thrust

Autor:	Yi Jiang, Rui Qing Liu
Rok vydání:	2014
Předmět:	Engineering Computer simulation business.industry General Engineering Thrust Flow field symbols.namesake Missile Mach number Physics::Space Physics Fluent symbols High Energy Physics::Experiment Rocket engine Aerospace engineering business Mach tuck
Zdroj:	Advanced Materials Research. :1331-1336
ISSN:	1662-8985
DOI:	10.4028/www.scientific.net/amr.1030-1032.1331
Popis:	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.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::d9224571c846151573baf6816b7dd15b https://doi.org/10.4028/www.scientific.net/amr.1030-1032.1331 Zobrazit plný text záznamu