Dynamic Pressure at Wing in Static Stability and Control Formulas

Dynamic Pressure at Wing Represents the kinetic energy per unit volume of air due to its motion. And is denoted by Q_w. Dynamic Pressure at Wing is usually measured using the Pascal for Pressure. Note that the value of Dynamic Pressure at Wing is always negative.

Static Stability and Control formulas that make use of Dynamic Pressure at Wing

fxYawing Moment Coefficient given Rudder DeflectionGo

fxRudder Deflection Angle given Yawing Moment CoefficientGo

fxYawing Moment given Rudder DeflectionGo

FAQ

What is the Dynamic Pressure at Wing?

Dynamic Pressure at Wing Represents the kinetic energy per unit volume of air due to its motion. Dynamic Pressure at Wing is usually measured using the Pascal for Pressure. Note that the value of Dynamic Pressure at Wing is always negative.

Can the Dynamic Pressure at Wing be negative?

Yes, the Dynamic Pressure at Wing, measured in Pressure can be negative.

What unit is used to measure Dynamic Pressure at Wing?

Dynamic Pressure at Wing is usually measured using the Pascal[Pa] for Pressure. Kilopascal[Pa], Bar[Pa], Pound Per Square Inch[Pa] are the few other units in which Dynamic Pressure at Wing can be measured.

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