| 1. | There is no position error associated with stagnation pressure.
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| 2. | This static pressure is called the stagnation pressure.
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| 3. | The dynamic pressure, then, is the difference between the stagnation pressure and the static pressure.
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| 4. | Bernoulli's principle states that total pressure ( or stagnation pressure ) is constant along a streamline.
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| 5. | The static pressure at the stagnation point is of special significance and is given its own name stagnation pressure.
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| 6. | There is no variation in stagnation pressure, regardless of the position on the streamline where it is measured.
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| 7. | The ratios for the pressure, density, temperature, velocity and stagnation pressure are shown below, respectively.
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| 8. | Depending on where the inlet holes are located on the probe, it can measure static pressures or stagnation pressures.
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| 9. | Stagnation properties ( e . g . stagnation temperature, stagnation pressure ) are useful in jet engine performance calculations.
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| 10. | The ratios for the pressure, density, static temperature, velocity and stagnation pressure are shown below, respectively.
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