((better)): Aircraft+propulsion+saeed+farokhi+solution+manual+top

For the high-pressure compressor and burner, the manual references the burner efficiency $\eta_b$ and uses the heating value of Jet-A ($Q_R = 43,400 \text kJ/kg$).

: Mathematical modeling of pressure recovery and thrust coefficients. Turbomachinery aircraft+propulsion+saeed+farokhi+solution+manual+top

Farokhi’s problems often require gas tables (air tables). The best solutions show exactly which table row was interpolated to find $h$, $p_r$, or $u$. For the high-pressure compressor and burner, the manual

Navigating Aircraft Propulsion: A Guide to Saeed Farokhi’s Seminal Work and Study Resources For the high-pressure compressor and burner