| 1. | The resulting pressure distribution is asymmetrical and is shifted to the right.
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| 2. | However, an experimental measurement of the corresponding surface pressure distribution is not known.
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| 3. | The average pressure can be obtained from the integral of the pressure distribution:
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| 4. | This solution gave the exact pressure distribution around an airfoil of arbitrary shape.
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| 5. | This spanwise-varying pressure distribution is sustained by a mutual interaction with the velocity field.
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| 6. | One is a non uniform pressure distribution among the material being pressed into the mold.
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| 7. | Ideally, the pressure distributions on the intersecting bodies should complement each other s pressure distribution.
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| 8. | Ideally, the pressure distributions on the intersecting bodies should complement each other s pressure distribution.
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| 9. | When this is the case, it is possible to assume that a hydrostatic pressure distribution applies.
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| 10. | The initial flights looked at longitudinal stability and control, wing and tail loads, and pressure distribution.
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