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Aircraft Mechanics
Lift with respect to Roll Rate in Static Stability and Control Formulas
Lift with respect to Roll Rate refers to the relationship between the lift force generated by an aircraft’s wings and the rate at which the aircraft rolls about its longitudinal axis. And is denoted by L. Lift with respect to Roll Rate is usually measured using the Newton for Force. Note that the value of Lift with respect to Roll Rate is always negative.
Formulas to find Lift with respect to Roll Rate in Static Stability and Control
f
x
Lift given Roll Rate
Go
List of variables in Static Stability and Control formulas
f
x
Lift Curve Slope
Go
f
x
Roll Rate
Go
f
x
Reference Velocity across X Axis
Go
f
x
Pitch Rate
Go
f
x
Chord
Go
f
x
Wingspan
Go
FAQ
What is the Lift with respect to Roll Rate?
Lift with respect to Roll Rate refers to the relationship between the lift force generated by an aircraft’s wings and the rate at which the aircraft rolls about its longitudinal axis. Lift with respect to Roll Rate is usually measured using the Newton for Force. Note that the value of Lift with respect to Roll Rate is always negative.
Can the Lift with respect to Roll Rate be negative?
Yes, the Lift with respect to Roll Rate, measured in Force can be negative.
What unit is used to measure Lift with respect to Roll Rate?
Lift with respect to Roll Rate is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Lift with respect to Roll Rate can be measured.
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