Author name: Aathif Muzain C

The “Mass of Struts” in aircraft design refers to the total mass of the struts that are part of the landing gear system of an aircraft. These struts provide structural support and shock absorption during landing, taxiing, and takeoff. Here’s the formula, definition, and SI unit for the Mass of Struts: Formula for Mass of […]

The “Mass of Wheels and Tires” in aircraft design refers to the combined mass of the wheels and tires used in the landing gear system of an aircraft. These components are crucial for supporting the aircraft’s weight during landing, taxiing, and takeoff. Here’s the formula, definition, and SI unit for the Mass of Wheels and

The “Mass of Nose Landing Gear” in aircraft design refers to the total mass of the landing gear components specifically located under the aircraft’s nose or forward section. This includes items such as the nose wheels, struts, brakes, tires, and associated structural elements for the nose landing gear. Here’s the formula, definition, and SI unit

The “Mass of Main Landing Gear” in aircraft design refers to the total mass of the landing gear components specifically located under the aircraft’s main wings. This includes items such as the wheels, struts, brakes, tires, and associated structural elements for the main landing gear. Here’s the formula, definition, and SI unit for the Mass

The “Weight of Other Structural Components” in aircraft design refers to the mass of various structural elements and components that are not part of the main airframe, wings, or landing gear but are essential for the aircraft’s operation and functionality. These components can include things like tail assemblies, engine mounts, fairings, and more. Here’s the

The “Weight of Landing Gear” in aircraft design refers to the total mass of the landing gear components, including wheels, struts, brakes, tires, and associated structural elements. The weight of the landing gear is an essential parameter in aircraft design, as it affects the overall weight and balance of the aircraft. Here’s the formula, definition,

The “Weight of Fuselage” in aircraft design refers to the mass of the aircraft’s main body or fuselage, which houses the cockpit, cabin, cargo compartments, and various essential systems and components. The weight of the fuselage is a significant factor in determining the aircraft’s overall weight and balance. Here’s the formula, definition, and SI unit

The “Weight of Wing” in aircraft design refers to the mass of the aircraft’s wings, including their supporting structures, control surfaces, and associated components. The weight of the wing is a critical parameter in aircraft design, as it directly affects the aircraft’s overall weight and balance. Here’s the formula, definition, and SI unit for the

The “Weight of Airframe” in aircraft design refers to the mass of the aircraft’s main supporting structure, excluding other major components like wings, engines, and landing gear. The airframe includes the fuselage, tail section, and any other structural elements that make up the aircraft’s framework. Here’s the formula, definition, and SI unit for the Weight

The Basic Structure Weight (BSW) in aircraft design refers to the weight of the fundamental structural components of the aircraft, which are essential for its integrity and functionality. These components include the airframe, wings, fuselage, landing gear, and other structural elements. BSW is a critical parameter in aircraft design, as it forms the foundation for