Zobrazeno 1 - 2
of 2
pro vyhledávání: '"H. R. Ali Mohammadi"'
Publikováno v:
فصلنامه علوم و فناوری فضایی, Vol 6, Iss 3, Pp 1-13 (2013)
In this paper, a particular propulsion system including, liquid rocket engine, fuel and oxidizer tank and related pressurizing system, have been surveyed. The procedure is based on a nonlinear mathematical model which has been simulated in Matlab Sim
Externí odkaz:
https://doaj.org/article/50e857f6e59a46159fcd6147823775e6
Autor:
M. Naghikhani, H. R. Ali Mohammadi
Publikováno v:
فصلنامه علوم و فناوری فضایی, Vol 4, Iss 1, Pp 61-67 (2011)
Selection of the optimal tolerance for the components is one of the most important and complex issues in the design of the parts and products especially in sensitive and accurate industries (like as aerospace). Generally the design engineers tend to
Externí odkaz:
https://doaj.org/article/0d432a99688b4fbcb6c8c1d64014fdf0