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