Power Required at Altitude in Introduction and Governing Equations Formulas

Power Required at Altitude is the power required for an aircraft to fly with a specific velocity at an altitude for a given altitude (or density). And is denoted by P_R,alt. Power Required at Altitude is usually measured using the Watt for Power. Note that the value of Power Required at Altitude is always positive.

Formulas to find Power Required at Altitude in Introduction and Governing Equations

fxPower required at AltitudeGo

fxPower required at Altitude given Power at sea-levelGo

List of variables in Introduction and Governing Equations formulas

fx Weight of Body Go

fx Drag Coefficient Go

fx Density Go

fx Reference Area Go

fx Lift Coefficient Go

fx Power Required at Sea-level Go

FAQ

What is the Power Required at Altitude?

Power Required at Altitude is the power required for an aircraft to fly with a specific velocity at an altitude for a given altitude (or density). Power Required at Altitude is usually measured using the Watt for Power. Note that the value of Power Required at Altitude is always positive.

Can the Power Required at Altitude be negative?

No, the Power Required at Altitude, measured in Power cannot be negative.

What unit is used to measure Power Required at Altitude?

Power Required at Altitude is usually measured using the Watt[W] for Power. Kilowatt[W], Milliwatt[W], Microwatt[W] are the few other units in which Power Required at Altitude can be measured.

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