October 2023

In aircraft design, “Power of Aircraft System” refers to the rate at which work is done or energy is transferred or converted within a specific system or component of the aircraft. Here’s the definition and SI unit for power in aircraft systems: Formula: The formula for calculating power (P) is based on the rate of […]

In aircraft systems and engineering, “frequency” typically refers to the measurement of how often a periodic event occurs within a specified time interval. Frequency is a fundamental parameter used in various aspects of aircraft systems, including avionics, communication systems, and navigation. Here’s the definition and SI unit for frequency in aircraft systems: Formula: Frequency is

In aircraft systems and electrical engineering, “resistance” refers to the property of a material or component that opposes the flow of electric current. Resistance is a fundamental parameter used in electrical calculations and circuit analysis. Here’s the definition and SI unit for resistance in aircraft systems: Formula: The formula for resistance (R) in an electrical

In aircraft systems and electrical engineering, “charge” refers to the quantity of electric charge, which is the fundamental property of matter responsible for electrical interactions. Electric charge is a key parameter in understanding and designing electrical systems. Here’s the definition and SI unit for charge in aircraft systems: Formula: The formula for electric charge (Q)

In aircraft electrical systems and engineering, “current” refers to the flow of electric charge through a conductor or electrical circuit. Current is a fundamental parameter for electrical systems, including those used in aircraft. Here’s the definition and SI unit for current in aircraft systems: Formula: The formula for current (I) in an electrical circuit is

Voltage in aircraft systems, as in electrical systems in general, is a crucial parameter that governs the flow of electrical energy and the operation of various equipment. Here’s the definition and SI unit for voltage in aircraft systems: Formula: Voltage is typically measured using a voltmeter, which provides a direct reading in volts (V). However,

In aircraft design, temperature within aircraft systems is a critical parameter that affects the performance and operation of various components. Here’s the definition and SI unit for temperature in aircraft systems: Formula: The formula for converting between degrees Celsius (°C) and kelvin (K) is straightforward:

In aircraft design, various systems use pressure to perform functions like hydraulic actuation, pneumatic control, and air conditioning. Here’s the definition and SI unit for pressure in aircraft systems: Formula: The formula for pressure (P) in a system can be defined as: P represents pressure in pascals (Pa). F is the force applied perpendicular to

In aircraft design, the density of a cargo compartment typically refers to the average density of the cargo or items being transported within that compartment. It’s important to note that the cargo compartment itself is typically constructed from lightweight materials like aluminum, and its density is relatively constant. Therefore, the density calculation usually pertains to

The mass of a cargo compartment in aircraft design is not typically calculated as a standalone parameter because it is considered part of the aircraft’s empty operating weight (EOW). EOW includes the weight of the aircraft’s structure, systems, and various components, including cargo compartments, when they are empty.However, if you have specific information about the