Author name: Kalpana Southri

 flight mechanics, the “load factor for minimum radius” refers to the load factor experienced by an aircraft when it is flying a steady turn at the minimum possible radius. This is often referred to as the “minimum radius turn” or “tightest turn” an aircraft can perform at a given airspeed Zero lift coefficient (Cd0) Thrust […]

In flight mechanics, the “climb phase” refers to a specific portion of an aircraft’s flight where it is ascending vertically in altitude, either after takeoff or during the initial phase of the flight. The climb phase is a critical part of an aircraft’s operation as it transitions from its takeoff phase to its desired cruising

In flight mechanics, the “minimum radius of turn” refers to the smallest radius that an aircraft can achieve during a steady turn at a given airspeed and bank angle. It represents the tightest possible turn the aircraft can execute without stalling or exceeding its structural limits. Wing loading (w/s) in kg/m^2 Thrust loading (Ta/w) in

In flight mechanics, the “radius of turn” refers to the distance from the center of a turn to the position of the aircraft at any given moment during a steady turn. It is the radius of the circular path followed by an aircraft as it turns. R is the radius of turn. v is the

In flight mechanics, potential energy refers to the energy possessed by an aircraft due to its position relative to the Earth’s surface. It is one of the two main forms of mechanical energy, the other being kinetic energy. Potential energy arises from the force of gravity acting on the aircraft. PE = m * g

In flight mechanics, “power required minimum” refers to the minimum amount of power needed by an aircraft to maintain a steady level flight at a specific airspeed and altitude. It is an essential concept in aircraft performance analysis and plays a significant role in determining an aircraft’s operational capabilities. The “power required” is the total

Equivalent Shaft Horsepower (ESHP) is a term used in flight mechanics to quantify the power output or power required of a propeller-driven aircraft engine. It represents the combination of the engine’s shaft horsepower (SHP) and the power required to drive the propeller. This concept is particularly relevant for aircraft with a propeller, as it considers

Flight mechanics refers to the process of defining the steps or actions that are performed by an aircraft during a flight simulation or test Cs = v / (ρ / ρn^2)^(1/5) where: Cs = Speed of sound v = Velocity of the aircraft ρ = Density of the air at the given altitude ρn =

n flight mechanics, “flight using thrust horsepower” refers to the process of analyzing and evaluating the performance of an aircraft based on the thrust generated by its engines, measured in horsepower. Thrust horsepower (THP) is the power output of the aircraft’s engines or propulsion system specifically in terms of the thrust produced. THP = (0.5

In flight mechanics, “power input” refers to the total power supplied to the aircraft’s propulsion system. It represents the energy consumed by the engines or any other propulsion devices to produce thrust and propel the aircraft through the air. Power input is a crucial parameter in assessing an aircraft’s performance, as it directly affects its