Examples of using Static pressure in English and their translations into Hebrew
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High Static Pressure(Central).
The airspeed indicator is connected to both the pitot and static pressure sources.
This static pressure is called the stagnation pressure. .
His vehicle weighs roughly 3,000 kilos, exerting a static pressure of 75 kilos per meter square.
For high static pressure, an industrial fan is the thing you want.
The dynamic pressure, then,is the difference between the stagnation pressure and the static pressure.
The static pressure is used in all measurements, while the pitot pressure is used only to determine airspeed.
The airspeed indicator works bycomparing dynamic pressure(ram air pressure) and static pressure.
High Static Pressure Duct Units, also known as central air, are ideal for large rooms and open floor plans.
The Bernoulli equation applicable to incompressible flow shows that the stagnationpressure is equal to the dynamic pressure plus static pressure.
When the static pressure increases or decreases, mechanical connections trigger the altimeter needle to show a corresponding altitude in feet.
It incorporates a second coaxial tube(or tubes) with pressure sampling holes on the sides of the probe, outside the direct airflow,to measure the static pressure.
External Static Pressure(ESP) adjusts the unit's fan speed so that your ideal ambience is achieved with a quieter, more efficient operation.
The filling method is the same as that of the first layer, and the static pressure of 25T roller is used for two times so that the reinforcement of the subgrade base is completed.
The new static pressure in the pitot tube would be equivalent to the static pressure from the static port, and the airspeed indicator would read"0.".
Total pressure is also equal to dynamic pressure plus static pressure so, in incompressible flows, stagnation pressure is equal to total pressure. .
Long-term static pressure on the spine can also be recalled by pain, which, however, passes if a person changes body position or prilazhet for several minutes.
If the pitot tube becomes blocked and the drain hole remains open, the ram air pressure will bleed out through the drain hole,leaving only static pressure in the pitot tube.
Velocity pressure, along with static pressure and pressure due to elevation, are used in Bernoulli's principle as an energy balance on a closed system.
Liquid column, such as U-tube pressure gauge, Pressure Gauge pipe pressure gauge, etc.,is based on the principle of fluid static pressure signal into a liquid column height signal, often use water, alcohol or mercury as a pressure gauge.
In the long run, the increase in static pressure in this region of the body is detrimental to the flow of blood through the veins, and the form of veins so that spider veins are a plausible result.
In fluid dynamics, a stagnation point is a point in a flow field where the local velocity of the fluid is zero.[1]:§ 3.2 Stagnation points exist at the surface of objects in the flow field, where the fluid is brought to rest by the object.The Bernoulli equation shows that the static pressure is highest when the velocity is zero and hence static pressure is at its maximum value at stagnation points. This static pressure is called the stagnation pressure.[2][1]:§ 3.5.
The dynamic pressure, along with the static pressure and the pressure due to elevation, is used in Bernoulli's principle as an energy balance on a closed system.
The new alternate static pressure is a lower pressure than outside ambient pressure during flight, which results in slightly inaccurate instrument indications, but it provides a good enough indication to maintain positive aircraft control.
The Bernoulli equation shows that the static pressure is highest when the velocity is zero andhence static pressure is at its maximum value at stagnation points.
Stagnation pressure minus freestream static pressure is equal to freestream dynamic pressure; therefore the pressure coefficient C p{\displaystyle C_{p}} at stagnation points is +1.[1]:§ 3.6.
If the air on one side of the diaphragm is at the static pressure, and the other at the stagnation pressure, then the deflection of the diaphragm is proportional to the dynamic pressure. .
In some aircraft, two ADCs receive total and static pressure from independent pitot tubes and static ports, and the aircraft's flight data computer compares the information from both computers and checks one against the other.
C p{\displaystyle C_{p}} is pressure coefficient p{\displaystyle p} is static pressure at the point at which pressure coefficient is being evaluated p∞{\displaystyle p_{\infty}} is static pressure atpoints remote from the body(freestream static pressure) q∞{\displaystyle q_{\infty}} is dynamic pressure at points remote from the body(freestream dynamic pressure).