Author name: Aathif Muzain C

In aircraft design and engineering, “T_outlet” represents the absolute temperature of the air at the inlet of a component or system, such as a compressor or an engine. Absolute temperature is typically measured in kelvin (K) or other temperature units. The formula for calculating the absolute temperature at the inlet (T_outlet) is based on the […]

In aircraft design and engineering, “T_inlet” represents the absolute temperature of the air at the inlet of a component or system, such as a compressor or an engine. Absolute temperature is typically measured in kelvin (K) or other temperature units. The formula for calculating the absolute temperature at the inlet (T_inlet) is based on the

In aircraft design and engineering, “T_inlet” represents the absolute temperature of the air at the inlet of a component or system, such as a compressor or an engine. Absolute temperature is typically measured in kelvin (K) or other temperature units. The formula for calculating the absolute temperature at the inlet (T_inlet) is based on the

In aircraft design and engineering, the “Isentropic Work Done” represents the work required or done during an idealized (isentropic) compression process within a compressor. It is a theoretical measure of the work required to achieve the compression of air under idealized conditions, assuming a reversible and adiabatic (no heat exchange with the surroundings) process. The

In aircraft design and engineering, the efficiency of a centrifugal flow compressor is a measure of how effectively the compressor increases the pressure of the incoming air while minimizing losses. It is typically expressed as the isentropic efficiency, which considers the idealized (isentropic) compression process. The isentropic efficiency (η_isen) of a centrifugal flow compressor can

The “number of revolutions” in aircraft design refers to the count of full rotations made by a rotating component over a specified period. This parameter is used to characterize the angular motion or rotation of various components within an aircraft, such as engine crankshafts, propellers, or rotor blades. The formula for calculating the number of

In aircraft design and engineering, “RPM” stands for “Revolutions Per Minute,” and it represents the rotational speed of a component, typically measured in the number of complete revolutions made by that component in one minute. RPM is a crucial parameter in aviation, as it’s used to characterize the speed of various rotating components within an

In aircraft design and engineering, “V_inlet” represents the velocity of the fluid (typically air) at the inlet of a component or system, such as a compressor, inlet duct, or air intake. The formula for calculating V_inlet can be defined as: V_inlet is the velocity of the fluid at the inlet, typically measured in meters per

In aircraft design and engineering, “V_outlet” represents the velocity of the fluid (typically air) at the outlet of a component or system, such as a compressor, nozzle, or exhaust. The formula for calculating V_outlet can be defined as: V_outlet is the velocity of the fluid at the outlet, typically measured in meters per second (m/s)

In aircraft design and engineering, “P_total_outlet” represents the total pressure at the outlet of a component or system, such as a compressor or a nozzle. Total pressure is a combination of both static pressure and dynamic pressure, and it is a crucial parameter used to assess the performance and behavior of various aircraft components. The