The Liquid Rocket Engine Design System Using a New Thermo-Gas-Dynamic Calculation Method.
| Autor: | ABDULLAYEV, Parviz1 a_parviz@mail.ru, ABDULLA, Nijat2 nijat.abdulla@mail.ru |
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| Zdroj: | Journal of Aeronautics & Space Technologies / Havacilik ve Uzay Teknolojileri Dergisi. Jul2019, Vol. 12 Issue 2, p171-183. 13p. |
| Databáze: | Academic Search Ultimate |
| Externí odkaz: |
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