These calculations, made at the request of the Zeppelin AirshipudCompany of Friederichshafen, Germany, were based on the shapeudof the ZR III, with the following simplifications:udcars, fins, and rudders removed; all cross sections replaced by equivalent circular cross sections. Under these assumptions the pressure distribution was calculated for the following cases: symmetrical case, or flow parallel to the axis; unsymmetrical case, or flow at an angle to the axis. In both cases the simple potential flow first forms the basis for the determination of the pressure distribution.
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