In 1923, the United States Army (there was no United States Air Force at that time) set a record for in-flight refueling of airplanes. Using two refueling planes, an Airco DH-4B biplane was able to remain in flight for 37 h . During the flight, the refueling planes were able to air-transfer a total of 687 gallons of fuel to the plane in 9 refueling transfers. Assume that the refueling nozzle had a diameter of 1.45 in and each refueling took 2.45 min to perform. Calculate the velocity of the fuel through the nozzle. Assume that the fuel filled the entire cross-sectional area of the nozzle.

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Answer:

Explanation:

Total time of transfer oil fuel = 2.45 x 9 = 22.05 minutes

= 22.05 x 60

= 1323 s

Total volume of ful transferred = 687 gallon

= .0037854 x 687

= 2.6 m³

radius of pipe = .5 x 1.45 inch

= .5 x 1.45 x 2.54 x 10⁻² m

r = .018415 m

cross sectional area

= π r²

a = 3.14 x .018415²

= 10.648 x 10⁻⁴ m²

If v be the velocity

volume of fuel coming out  a x v x t  , a is cross sectional area , v is velocity and t is time .

10.648 x 10⁻⁴ x v x 1323  = 2.6

v = 1.845 m / s

This question involves the concepts of volume flow rate, flow speed, and cross-sectional area.

The velocity of fuel through the nozzle is "1.09 m/s".

The flow speed of fuel can be found using the formula for the volume flow rate of fuel:

[tex]\frac{V}{t}=Av\\\\V = Avt\\\\v = \frac{At}{V}[/tex]

where,

v = flow speed = ?

A = cross-sectional area = π(radius)² = π(1.45/2 in)²[tex](\frac{0.0254\ m}{1\ in})^2[/tex] = 0.0022 m²

t = time taken for refueling = (9)(2.45 min) = 22.05 min = 1323 s

V = Volume of fuel transferred = (687 gallons)[tex](\frac{0.003785 \ m^3}{1\ gallon})[/tex] = 2.6 m³

Therefore,

[tex]v=\frac{(0.0022\ m^3)(1323\ s)}{2.6\ m^3}\\\\[/tex]

v = 1.09 m/s

Learn more about volume flow rate here:

https://brainly.com/question/23127034?referrer=searchResults

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