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Average Value Range Equation Formula

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The Average Value Range Equation is to estimate an aircraft’s range. Range is simply aircraft velocity times endurance. Check FAQs

R AVG = \frac{Δw f}{c t \cdot (\frac{F D}{V})}

R_AVG - Average Value Range Equation?Δw_f - Change in Weight?c_t - Thrust-Specific Fuel Consumption?F_D - Drag Force?V - Flight Velocity?

Average Value Range Equation Example

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Here is how the Average Value Range Equation equation looks like with Values.

Here is how the Average Value Range Equation equation looks like with Units.

Here is how the Average Value Range Equation equation looks like.

151327.4336 = \frac{300}{10.17 \cdot (\frac{80}{114})}

151327.4336m = \frac{300kg}{10.17kg/h/N \cdot (\frac{80N}{114m/s})}

151327.4336 = \frac{300}{10.17 \cdot (\frac{80}{114})}

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Average Value Range Equation Solution

Follow our step by step solution on how to calculate Average Value Range Equation?

FIRST Step Consider the formula

R AVG = \frac{Δw f}{c t \cdot (\frac{F D}{V})}

Next Step Substitute values of Variables

∴

R AVG = \frac{300kg}{10.17kg/h/N \cdot (\frac{80N}{114m/s})}

Next Step Convert Units

∴

R AVG = \frac{300kg}{0.0028kg/s/N \cdot (\frac{80N}{114m/s})}

Next Step Prepare to Evaluate

∴

R AVG = \frac{300}{0.0028 \cdot (\frac{80}{114})}

Next Step Evaluate

∴

R AVG = 151327.433628319m

LAST Step Rounding Answer

∴

R AVG = 151327.4336m

Average Value Range Equation Formula Elements

Variables

Average Value Range Equation

The Average Value Range Equation is to estimate an aircraft’s range. Range is simply aircraft velocity times endurance.

Symbol: R_AVG

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Average Value Range Equation

Change in Weight

Change in Weight refers to the difference in initial and the final weight.

Symbol: Δw_f

Measurement: WeightUnit: kg

Note: Value can be positive or negative.

Formulas to find Change in Weight

Thrust-Specific Fuel Consumption

Thrust-Specific Fuel Consumption (TSFC) is the fuel efficiency of an engine design with respect to thrust output.

Symbol: c_t

Measurement: Thrust Specific Fuel ConsumptionUnit: kg/h/N

Note: Value should be greater than 0.

Formulas to find Thrust-Specific Fuel Consumption

Drag Force

Drag Force is the resisting force experienced by an object moving through a fluid.

Symbol: F_D

Measurement: ForceUnit: N

Note: Value can be positive or negative.

Formulas to find Drag Force

Flight Velocity

Flight Velocity is the speed with which the aircraft moves through the air.

Symbol: V

Measurement: SpeedUnit: m/s

Note: Value can be positive or negative.

Formulas to find Flight Velocity

Other formulas in Jet Airplane category

Go Endurance of Jet Airplane

E = C L \cdot \frac{\ln (\frac{W 0}{W 1})}{C D \cdot c t}

Go Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane

c t = C L \cdot \frac{\ln (\frac{W 0}{W 1})}{C D \cdot E}

Go Endurance for given Lift-to-Drag Ratio of Jet Airplane

E = (\frac{1}{c t}) \cdot LD \cdot \ln (\frac{W 0}{W 1})

Go Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag Ratio of Jet Airplane

c t = (\frac{1}{E}) \cdot LD \cdot \ln (\frac{W 0}{W 1})

How to Evaluate Average Value Range Equation?

Average Value Range Equation evaluator uses Average Value Range Equation = Change in Weight/(Thrust-Specific Fuel Consumption*(Drag Force/Flight Velocity)) to evaluate the Average Value Range Equation, The Average Value Range Equation calculates the average value of the aircraft range, this formula determines the average value based on the change in weight, the thrust-specific fuel consumption at the end of the range, the drag force at the end of the range, and the flight velocity at the end of the range. Average Value Range Equation is denoted by R_AVG symbol.

How to evaluate Average Value Range Equation using this online evaluator? To use this online evaluator for Average Value Range Equation, enter Change in Weight (Δw_f), Thrust-Specific Fuel Consumption (c_t), Drag Force (F_D) & Flight Velocity (V) and hit the calculate button.

FAQs on Average Value Range Equation

What is the formula to find Average Value Range Equation?

The formula of Average Value Range Equation is expressed as Average Value Range Equation = Change in Weight/(Thrust-Specific Fuel Consumption*(Drag Force/Flight Velocity)). Here is an example- 151327.4 = 300/(0.002825*(80/114)).

How to calculate Average Value Range Equation?

With Change in Weight (Δw_f), Thrust-Specific Fuel Consumption (c_t), Drag Force (F_D) & Flight Velocity (V) we can find Average Value Range Equation using the formula - Average Value Range Equation = Change in Weight/(Thrust-Specific Fuel Consumption*(Drag Force/Flight Velocity)).

Can the Average Value Range Equation be negative?

No, the Average Value Range Equation, measured in Length cannot be negative.

Which unit is used to measure Average Value Range Equation?

Average Value Range Equation is usually measured using the Meter[m] for Length. Millimeter[m], Kilometer[m], Decimeter[m] are the few other units in which Average Value Range Equation can be measured.

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Average Value Range Equation Formula

Average Value Range Equation Example

Average Value Range Equation Solution

Average Value Range Equation Formula Elements

Other formulas in Jet Airplane category

How to Evaluate Average Value Range Equation?

FAQs on Average Value Range Equation

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