TI  - Introducing an optimal pressure ratio for aircraft design and investigating the effect of nozzle efficiency on the jet engine’s performance
AU  - SIYAHI, H.
AU  - SIYAHI, M.
AU  - FALLAH, M.
AU  - MOHAMMADI, Z.
SO  - Journal of Thermal Engineering 2026;12:182-191.
DO  - 10.14744/thermal.0001072