| 11. | Thus the reduction in kinetic energy is countered by an increase in static pressure energy.
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| 12. | The flow of air through the venturi creates a reduced static pressure in the venturi.
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| 13. | The dynamic pressure, then, is the difference between the stagnation pressure and the static pressure.
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| 14. | Static pressure and temperature appear as fixed coefficients defined by convention as standard sea level values.
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| 15. | When gas velocity goes down the dynamic pressure is reduced, while the static pressure is increased.
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| 16. | This static pressure is called the stagnation pressure.
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| 17. | This increases the seat pressure of the valve ( the static pressure that holds the valve closed ).
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| 18. | In aircraft, The static pressure is generally measured using the static ports on the side of the fuselage.
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| 19. | Many authors refer to the pressure as static pressure to distinguish it from total pressure and dynamic pressure.
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| 20. | At low speeds ( subsonic speeds ) increases in static pressure are however limited to a few percent.
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