Verification of Model of Calculation of Intra-Chamber Parameters In Hybrid Solid-Propellant Rocket Engines; MATEC Web of Conferences; Vol. 72 : Heat and Mass Transfer in the System of Thermal Modes of Energy – Technical and Technological Equipment (HMTTSC-2016)

Verification of Model of Calculation of Intra-Chamber Parameters In Hybrid Solid-Propellant Rocket Engines

Bibliographic Details
Parent link:	MATEC Web of Conferences Vol. 72 : Heat and Mass Transfer in the System of Thermal Modes of Energy – Technical and Technological Equipment (HMTTSC-2016).— 2016.— [01135, 4 p.]
Corporate Author:	Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра теоретической и промышленной теплотехники (ТПТ)
Other Authors:	Zhukov I. S. Ilya, Borisov B. V. Boris Vladimirovich, Bondarchuk S. S. Sergey, Zhukov A. S. Alexander
Summary:	Title screen On the basis of obtained analytical estimate of characteristics of hybrid solid-propellant rocket engine verification of earlier developed physical and mathematical model of processes in a hybrid solid-propellant rocket engine for quasi-steady-state flow regime was performed. Comparative analysis of calculated and analytical data indicated satisfactory comparability of simulation results.
Language:	English
Published:	2016
Subjects:	электронный ресурс труды учёных ТПУ твердотопливные ракетные двигатели ракетные двигатели физико-математические модели квазистационарный режим
Online Access:	http://dx.doi.org/10.1051/matecconf/20167201135 http://earchive.tpu.ru/handle/11683/33504
Format:	Electronic Book Chapter
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=650005

Internet

http://dx.doi.org/10.1051/matecconf/20167201135
http://earchive.tpu.ru/handle/11683/33504