Aerospace Calculator

Stick force refers to the force exerted on the control stick or yoke by the pilot to adjust the elevator control surface and, consequently, the aircraft’s pitch attitude. It is the feedback experienced by the pilot when applying input to the elevator control. Stick force characteristics, including the required force for a given pitch change, […]

In flight mechanics, the elevator area  represents the effective aerodynamic surface area of the horizontal stabilizer’s elevator control surface. It plays a crucial role in controlling the pitch motion of an aircraft. Denoted as Se, it is used in aerodynamic calculations and equations to determine elevator effectiveness and its contribution to pitch control. The elevator,

The yawing moment in flight mechanics refers to the rotational force acting around the aircraft’s vertical axis, influencing its heading. It occurs due to asymmetries in aerodynamic forces, such as uneven thrust, crosswinds, or control surface deflections. This rotational motion influences the aircraft’s heading and requires corrective actions from the pilot, typically using the rudder.

In flight mechanics, the velocity for a pull-down maneuver refers to the airspeed necessary for an aircraft to descend while executing a controlled pitch movement. It is determined by factors such as the desired pitch rate, gravitational force, and the specific characteristics of the maneuver. This velocity is essential for pilots to effectively manage and

In flight mechanics, the velocity for a pull-up maneuver is the speed required for the aircraft to follow a curved trajectory, influenced by the centripetal force needed to balance lift and weight. The maneuver’s radius, describing the curvature of the path, affects this relationship. The lift force during a pull-up equals the aircraft’s weight plus

The Velocity Given By Pull-Up Maneuver Rate is a parameter in flight mechanics that describes the rate at which an aircraft’s velocity increases during a pull-up maneuver. It quantifies the change in velocity as the aircraft transitions from level flight to an upward trajectory. This rate is crucial for assessing the aircraft’s ability to climb

In a pull-down maneuver, the velocity refers to the speed at which an aircraft descends during the maneuver. When executing a pull-down, the aircraft transitions from level or climbing flight to a descending trajectory. The velocity attained during this maneuver depends on factors such as the aircraft’s initial altitude, angle of descent, aerodynamic characteristics, and

The sideslip angle (β) is the angle formed between the aircraft’s longitudinal axis and the relative wind, indicating the degree of lateral deviation from coordinated flight. The sideslip angle is crucial for controlling aerodynamic forces during maneuvers like slips and skids. Pilots rely on this information to maintain coordinated flight, especially in situations where wind

Wing area is the total surface area of an aircraft’s wings that is exposed to the oncoming air during flight. It is a critical parameter in determining the aerodynamic characteristics and performance of an aircraft. Wing area is typically measured in square units, such as square feet or square meters, and it plays a key