Formula Used:
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The Elevator Chord Length is the chord length of an elevator measured from its hinge line to trailing edge. It is a critical parameter in aircraft control surface design that affects the hinge moment and control forces required.
The calculator uses the formula:
Where:
Explanation: This formula calculates the elevator chord length based on the hinge moment, aerodynamic coefficients, flight conditions, and elevator geometry.
Details: Accurate calculation of elevator chord length is crucial for aircraft control system design, ensuring proper control forces, stability, and maneuverability characteristics.
Tips: Enter hinge moment in N·m, hinge moment coefficient, density in kg/m³, flight velocity in m/s, and elevator area in m². All values must be positive and valid.
Q1: What is the significance of hinge moment coefficient?
A: The hinge moment coefficient represents the aerodynamic characteristics of the control surface and affects the control forces required by the pilot.
Q2: How does flight velocity affect elevator chord length?
A: Higher flight velocities generally require smaller elevator chord lengths to maintain the same hinge moment, as the dynamic pressure increases with velocity squared.
Q3: What are typical values for elevator chord length?
A: Elevator chord length varies by aircraft type but typically ranges from 20-40% of the horizontal stabilizer chord length.
Q4: How does density affect the calculation?
A: Higher air density increases the dynamic pressure, which affects the hinge moment and consequently the required elevator chord length.
Q5: Can this calculator be used for other control surfaces?
A: While the principle is similar, different control surfaces may have different aerodynamic characteristics and would require appropriate coefficients.