Computational investigation of cooling effectiveness for film cooled dual-bell exhaust nozzle for LO2/LH2 liquid rocket engines

Autor:	David Šimurda, Abhilash Suryan, Martin Raju
Rok vydání:	2021
Předmět:	Fuel Technology Materials science Nuclear Energy and Engineering Renewable Energy Sustainability and the Environment Liquid-propellant rocket Nozzle Energy Engineering and Power Technology Bell nozzle Mechanics Propelling nozzle Dual (category theory)
Zdroj:	Energy Sources, Part A: Recovery, Utilization, and Environmental Effects. :1-17
ISSN:	1556-7230 1556-7036
DOI:	10.1080/15567036.2021.1963885
Popis:	A dual bell nozzle (DBN) consists of two bell nozzles of different geometric area ratios attached at the region called inflection. This distinct geometry modification allows the nozzle to adapt to ...
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::1db7d499939c1f0099b1f4b3cfa8f69e https://doi.org/10.1080/15567036.2021.1963885 Zobrazit plný text záznamu