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Aircraft Mechanics
Dihedral angle in Static Stability and Control Formulas
The dihedral angle is defined as the spanwise inclination of the wing with respect to the horizontal. And is denoted by Γ. Dihedral angle is usually measured using the Radian for Angle. Note that the value of Dihedral angle is always negative.
Formulas to find Dihedral angle in Static Stability and Control
f
x
Dihedral angle for given sideslip velocity
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Static Stability and Control formulas that make use of Dihedral angle
f
x
Normal component of aircraft side velocity for given dihedral angle
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f
x
Aircraft sideslip velocity for given dihedral angle
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List of variables in Static Stability and Control formulas
f
x
Side Velocity Normal Component
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f
x
Sideslip velocity
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FAQ
What is the Dihedral angle?
The dihedral angle is defined as the spanwise inclination of the wing with respect to the horizontal. Dihedral angle is usually measured using the Radian for Angle. Note that the value of Dihedral angle is always negative.
Can the Dihedral angle be negative?
Yes, the Dihedral angle, measured in Angle can be negative.
What unit is used to measure Dihedral angle?
Dihedral angle is usually measured using the Radian[rad] for Angle. Degree[rad], Minute[rad], Second[rad] are the few other units in which Dihedral angle can be measured.
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