Fx Copy
LaTeX Copy
Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft. Check FAQs
Pexcess=RCW
Pexcess - Excess Power?RC - Rate of Climb?W - Aircraft Weight?

Excess power for given rate of climb Example

With values
With units
Only example

Here is how the Excess power for given rate of climb equation looks like with Values.

Here is how the Excess power for given rate of climb equation looks like with Units.

Here is how the Excess power for given rate of climb equation looks like.

37197.6Edit=3.7198Edit10000Edit
You are here -
HomeIcon Home » Category Physics » Category Aerospace » Category Aircraft Mechanics » fx Excess power for given rate of climb

Excess power for given rate of climb Solution

Follow our step by step solution on how to calculate Excess power for given rate of climb?

FIRST Step Consider the formula
Pexcess=RCW
Next Step Substitute values of Variables
Pexcess=3.7198m/s10000N
Next Step Prepare to Evaluate
Pexcess=3.719810000
LAST Step Evaluate
Pexcess=37197.6W

Excess power for given rate of climb Formula Elements

Variables
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.
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.

Other Formulas to find Excess Power

​Go Excess power
Pexcess=v(T-FD)

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 Weight of Aircraft for given Excess Power
W=PexcessRC

How to Evaluate Excess power for given rate of climb?

Excess power for given rate of climb evaluator uses Excess Power = Rate of Climb*Aircraft Weight to evaluate the Excess Power, Excess power for given rate of climb refers to the additional power available to an aircraft beyond what is necessary to maintain a specific climb rate under prevailing flight conditions, it's a measure of the aircraft's ability to climb at a specified rate while still having power available for other purposes, such as accelerating or maneuvering. Excess Power is denoted by Pexcess symbol.

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

FAQs on Excess power for given rate of climb

What is the formula to find Excess power for given rate of climb?
The formula of Excess power for given rate of climb is expressed as Excess Power = Rate of Climb*Aircraft Weight. Here is an example- 37170 = 3.71976*10000.
How to calculate Excess power for given rate of climb?
With Rate of Climb (RC) & Aircraft Weight (W) we can find Excess power for given rate of climb using the formula - Excess Power = Rate of Climb*Aircraft Weight.
What are the other ways to Calculate Excess Power?
Here are the different ways to Calculate Excess Power-
  • Excess Power=Velocity*(Thrust-Drag Force)OpenImg
Can the Excess power for given rate of climb be negative?
No, the Excess power for given rate of climb, measured in Power cannot be negative.
Which unit is used to measure Excess power for given rate of climb?
Excess power for given rate of climb is usually measured using the Watt[W] for Power. Kilowatt[W], Milliwatt[W], Microwatt[W] are the few other units in which Excess power for given rate of climb can be measured.
Copied!