Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Парвиз Шахмурад оглы Абдуллаев"'
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 8, Pp 28-38 (2019)
Analysis of the thermodynamic and thermophysical properties of combustion products (CP) in the liquid rocket engine (LRE) chamber shows that their dissociation degree depends on temperature T, gas expansion degree ε, etc. Practically, CP’s are alw
Externí odkaz:
https://doaj.org/article/66a00a15f444450bacf8135b49feafcc
