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Basics of gas turbines (15)

- Enthalpy of ideal gas at given temperature
- Heat capacity ratio
- Internal Energy of a perfect gas at given temperature
- Mach Angle
- Mach Number
- Mass flow rate of exhaust gases
- Mass flow rate of exhaust gases if fuel air ratio is known
- Pressure ratio
- Shaft work in compressible flow machines
- Shaft work in compressible flow machines neglecting inlet and exit velocities
- 5 More formulas!

Fundamentals of rotating machines (9)

- Degree of reaction for compressor
- Degree of reaction for turbine
- Impeller outlet diameter
- Isentropic efficiency of compression machine
- Isentropic efficiency of expansion machine
- Mean diameter of impeller
- Tip velocity of impeller if mean diameter is known
- Tip velocity of impeller in terms of hub diameter and inlet diameter
- Work done by roots blower

General fluid dynamics (8)

- Angular moment of momentum at exit
- Angular moment of momentum at inlet
- Energy transfer due to centrifugal effect
- Energy transfer due to change of absolute kinetic energy of the fluid
- Energy transfer due to the change of the relative kinetic energy of the fluid
- Peripheral velocity of the blade at the entry corresponding to diameter
- Peripheral velocity of the blade at the exit corresponding to diameter
- Torque produced

Gas cycles

Ideal cycles (9)

- Amount of heat added in simple gas turbine cycle
- Amount of heat added in simple gas turbine cycle if temperature is known
- Compressor work
- Compressor work in simple gas turbine if temperature is known
- Efficiency of a Joule cycle
- Efficiency of cycle
- Net work output in simple gas turbine cycle
- Turbine work in simple gas turbine cycle
- Turbine work in simple gas turbine cycle if temperature is known

Practical cycles (8)

- Efficiency of compressor in actual gas turbine cycle
- Efficiency of compressor in actual gas turbine cycle in terms of enthalpy
- Efficiency of turbine in actual gas turbine cycle
- Efficiency of turbine in actual gas turbine cycle in terms of enthalpy
- Minimum temperature ratio
- Stagnation enthalpy
- Work ratio in practical cycle
- Work required to drive the compressor including mechanical losses

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