DETERMINATION OF STATIC, VELOCITY AND TOTAL PRESSURE USING MANOMETERS AND PITOT TUBE Flashcards

1
Q

The pitot tube was invented by

A

Henri Pitot

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2
Q

, Bernoulli’s equation states

A

Stagnation pressure = static pressure + dynamic pressure

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3
Q

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)

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4
Q

t is the analysis of an applied force by a fluid (liquid or gas) on a
surface. Pressure is typically measured in units of force per unit of surface area. Many
techniques have been developed for the measurement of pressure and vacuum.

A

Pressure measurement

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5
Q

directional component of pressure in a moving

fluid is

A

dynamic pressure

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6
Q

is a device used to measure the fluid flow measurement invented by Henri
Pitot, a French engineer in 18th century.
It is widely to measure the airspeed of aircrafts, speedboat speed and for fluid flow
measurement in industrial application. Pitot tube measures the pressure point in
contact.

A

Pitot tube

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7
Q

Advantages of pitot tube.

A

Small and do not contain any moving parts
Low cost
Low permanent pressure loss.
Ease of installation into an existing system

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8
Q

Disadvantages of pitot tube

A

Foreign material in a fluid can easily clog pitot tube and disrupt normal reading as a result.
Low accuracy
Low rangeability

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9
Q

is also a measure of the amount that fluid pressure exceeds local
atmospheric pressure, but it includes the effect of the fluid velocity converted to
pressure. It is measured through a flat opening that is perpendicular to the direction of
fluid flow and facing into the fluid flow.

A

Stagnation pressure

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10
Q

l

A

l

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11
Q

is used to determine
changes in air pressure that occur as the aircraft’s altitude changes. must be calibrated prior to flight to register the pressure as an altitude above
sea level. T

A

pressure altimeter, also known as the barometric altimeter

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12
Q

is used to show the ratio of true airspeed in relation to the speed of sound.

A

machmeter

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13
Q

is the pitot-static instrument used to determine whether or not an aircraft
is flying in level flight.[4] The vertical speed specifically shows the rate of climb or the
rate of descent, which is measured in feet per minute or meters per second.[4] The
vertical speed is measured through a mechanical linkage to a diaphragm located within
the instrument

A

variometer

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