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Pitot Tube - Aerodynamics MCQ Questions

Pitot Tube MCQs : Here you will find MCQ Questions related to "Pitot Tube" in Aerodynamics. These Pitot Tube MCQ Questions Will help you to improve your Aerodynamics knowledge and will prepare you for various Examinations like Competitive Exams, Placements, Interviews and other Entrance Exmaniations




Question 1

A pitot tube, also known as?

A. pitot flow
B. pitot device
C. pitot probe
D. pitot boat

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Question 2

For the formula, Stagnation pressure equal to?

A. static pressure * dynamic pressure
B. static pressure - dynamic pressure
C. static pressure % dynamic pressure
D. static pressure + dynamic pressure

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Question 3

How many types of Pitot tube there?

A. 2
B. 3
C. 4
D. 5

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Question 4

In aircraft, the static pressure is generally measured using the static ports on the side of the fuselage

A. TRUE
B. FALSE
C. Can be true or false
D. Can not say

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Question 5

The fluid flow rate in a duct can then be estimated from?

A. Volume flow rate (cubic feet per minute) = duct area (square feet) + flow velocity (feet per minute)
B. Volume flow rate (cubic feet per minute) = duct area (square feet) - flow velocity (feet per minute)
C. Volume flow rate (cubic feet per minute) = duct area (square feet) × flow velocity (feet per minute)
D. Volume flow rate (cubic feet per minute) = duct area (square feet) / flow velocity (feet per minute)

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Question 6

In aviation, airspeed is typically measured in?

A. meter^2
B. cubicmeter
C. watt
D. knots

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Question 7

If a liquid column manometer is used to measure the pressure difference

A. TRUE
B. FALSE
C. Can be true or false
D. Can not say

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Question 8

____________ is the measure of purely random motion of the molecules of the gas.

A. Stagnation pressure
B. Static pressure
C. Dynamic pressure
D. Absolute pressure

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Question 9

How does the pitot tube help in measuring the airspeed?

A. Using temperature
B. Using the pressure difference
C. Using velocity
D. Using mach number

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Question 10

When the local flow velocity is zero itself then _________

A. 0
B. infinity
C. total pressure is not equal to static pressure
D. total pressure is equal to static pressure

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