Examination of a hypothetical 122 mm projectile reduced model in the supersonic wind tunnel

Autor:	Slobodan Vučković, Dušan Regodić
Jazyk:	angličtina
Rok vydání:	1996
Předmět:	mach number aerodynamics trisonic wind tunnel pressure center components of aerodynamic force and moments Military Science Engineering (General). Civil engineering (General) TA1-2040
Zdroj:	Vojnotehnički Glasnik, Vol 44, Iss 2, Pp 168-176 (1996)
Druh dokumentu:	article
ISSN:	0042-8469 2217-4753
DOI:	10.5937/VojTehG9602168V
Popis:	From the exterior ballistics aspect, it is necessary to reduce projectile overall resistance during the flight in order to attain longer range. Projectile overall resistance can be reduced by optimizing its dimensions and shapes. This paper presents the effects of dimensions and shapes of the rear part of a hypothetical 122 mm projectile reduced model on the total aerodynamic resistance coefficient. The model is examined in the trisonic wind tunnel T-36.
Databáze:	Directory of Open Access Journals
Externí odkaz:	https://doaj.org/article/4487fecd1d8244e89ee95ece00396d7d Zobrazit plný text záznamu View record in DOAJ