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Estimated Differential-Pressure Distribution over Fin for Maximum Fin Loading Condition

机译:最大翅片载荷条件下翅片的估计差压分布

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In order to design an antenna mount to be placed along the trailing edge of an A-3B fin in the yaw plane it is necessary to know the maximum differential pressure between the two sides of the fin which will occur there. An estimate has been made of the spanwise variation of the differential pressure at the mean Chordwise location of the antenna mount. Supplemental to this calculation the differential pressures were also obtained at three other Chordwise locations.

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