Weight of Aircraft for given Excess Power Formula

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Aircraft Weight is the total aircraft weight at any moment during the flight or ground operation. Check FAQs
W=PexcessRC
W - Aircraft Weight?Pexcess - Excess Power?RC - Rate of Climb?

Weight of Aircraft for given Excess Power Example

With values
With units
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Here is how the Weight of Aircraft for given Excess Power equation looks like with Values.

Here is how the Weight of Aircraft for given Excess Power equation looks like with Units.

Here is how the Weight of Aircraft for given Excess Power equation looks like.

10000Edit=37197.6Edit3.7198Edit
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Weight of Aircraft for given Excess Power Solution

Follow our step by step solution on how to calculate Weight of Aircraft for given Excess Power?

FIRST Step Consider the formula
W=PexcessRC
Next Step Substitute values of Variables
W=37197.6W3.7198m/s
Next Step Prepare to Evaluate
W=37197.63.7198
LAST Step Evaluate
W=10000N

Weight of Aircraft for given Excess Power Formula Elements

Variables
Aircraft Weight
Aircraft Weight is the total aircraft weight at any moment during the flight or ground operation.
Symbol: W
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Excess Power
Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft.
Symbol: Pexcess
Measurement: PowerUnit: W
Note: Value should be greater than 0.
Rate of Climb
The Rate of Climb (RoC) is defined as the aircraft's vertical speed – the positive or negative rate of altitude change with respect to time.
Symbol: RC
Measurement: SpeedUnit: m/s
Note: Value should be greater than 0.

Other formulas in Climbing Flight category

​Go Rate of Climb
RC=vsin(γ)
​Go Flight path angle at given rate of climb
γ=asin(RCv)
​Go Velocity of aircraft at given rate of climb
v=RCsin(γ)
​Go Excess power for given rate of climb
Pexcess=RCW

How to Evaluate Weight of Aircraft for given Excess Power?

Weight of Aircraft for given Excess Power evaluator uses Aircraft Weight = Excess Power/Rate of Climb to evaluate the Aircraft Weight, The Weight of Aircraft for given Excess Power refers to the force exerted by gravity on the mass of the aircraft, it's the sum of the mass of all components of the aircraft, including the airframe, payload (passengers, cargo), fuel, and any other items onboard, this equation suggests that the weight of the aircraft can be calculated based on the excess power available during climb flight and the rate of climb. Aircraft Weight is denoted by W symbol.

How to evaluate Weight of Aircraft for given Excess Power using this online evaluator? To use this online evaluator for Weight of Aircraft for given Excess Power, enter Excess Power (Pexcess) & Rate of Climb (RC) and hit the calculate button.

FAQs on Weight of Aircraft for given Excess Power

What is the formula to find Weight of Aircraft for given Excess Power?
The formula of Weight of Aircraft for given Excess Power is expressed as Aircraft Weight = Excess Power/Rate of Climb. Here is an example- 10007.43 = 37197.6/3.71976.
How to calculate Weight of Aircraft for given Excess Power?
With Excess Power (Pexcess) & Rate of Climb (RC) we can find Weight of Aircraft for given Excess Power using the formula - Aircraft Weight = Excess Power/Rate of Climb.
Can the Weight of Aircraft for given Excess Power be negative?
No, the Weight of Aircraft for given Excess Power, measured in Force cannot be negative.
Which unit is used to measure Weight of Aircraft for given Excess Power?
Weight of Aircraft for given Excess Power is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Weight of Aircraft for given Excess Power can be measured.
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