October 2023

Total Pressure (Pt), in the context of aircraft design and aviation, represents the sum of static pressure and dynamic pressure. It is often measured using a Pitot tube, which is a device that faces into the oncoming airflow to capture the total pressure. The formula for total pressure is: Pt is the total pressure. Ps […]

The Pitot pressure (Pp) is a pressure measurement taken at the front of a Pitot tube on an aircraft. It’s used to measure the total pressure experienced by the aircraft as it moves through the air. The formula for Pitot pressure is: Pp is the Pitot pressure. Total Pressure is the total pressure measured at

Static pressure in aircraft design is the pressure exerted by the still or undisturbed air surrounding the aircraft. It is an important parameter used in various aspects of aviation, including the calculation of altitude and airspeed. The formula to calculate static pressure is: P is the static pressure (in pascals, Pa). ρ (rho) is the

The airspeed indicator in aircraft design measures the speed of the aircraft through the air. The formula to calculate indicated airspeed (IAS) is: IAS is the indicated airspeed (in knots or other airspeed units). P is the dynamic pressure (in pascals or pounds per square foot), which is usually obtained from the pitot-static system. ρ

In aircraft design and electrical engineering, “Inductance (L)” refers to a property of electrical components, typically inductors, that measures their ability to store electrical energy in the form of a magnetic field when current flows through them. Inductance is a fundamental parameter used in the design of electrical circuits and systems, including those in aircraft.

In aircraft design and electrical engineering, “Capacity” or “Capacitance (C)” refers to the ability of a component, usually a capacitor, to store electrical charge and electrical energy. Capacitance is a fundamental parameter used in the design of electrical circuits and systems, including those in aircraft. Here’s the definition and SI unit for capacitance: Formula: The

In aircraft design and electrical engineering, “Resistance per unit length (ρ)” is a parameter that quantifies the resistance of a conducting material, such as a wire or cable, per unit of its length. It’s an important consideration when designing electrical circuits and systems to ensure that the desired electrical properties are achieved over specific distances.

In aircraft design and engineering, “Acceleration” refers to the rate of change of velocity of an aircraft or a specific object within an aircraft system. It’s a fundamental parameter used for analyzing motion, forces, and performance in aircraft systems. Here’s the definition and SI unit for acceleration in aircraft systems: Formula: The formula for calculating

In aircraft design and engineering, “Force (F)” is a fundamental physical quantity that represents a push or pull acting on an object. It’s a crucial parameter used to analyze and design various systems and components within an aircraft. Here’s the definition and SI unit for force in aircraft systems: Formula: The formula for calculating force

In aircraft design and engineering, the concept of “Work of Aircraft System” refers to the energy expended or transferred by a specific system or component within the aircraft while performing a task. Work is a measure of the effort or energy required to accomplish a particular function or operation. Here’s the definition and SI unit