The Pressure Distribution over the Horizontal Tail Surfaces of an Airplane III (1923)
NASA Technical Reports Server (NTRS) · leaf 7
. For the range of pressures used the deflection was proportional to the pressures and the effect of hysteresis wa,s quite negligible. One of the extra capsules was connected to a Mark IV Pitot head on the right-hand inner strut. On the corresponding left-hand strut was a similar head connected to… … Fig. 5.—Location of the pressure holes on the tail surface THE TAIL SURFACE. The tail surface used was of the standard .IN Hi type with a distribution of holes as shown in figure 5. It might be thought that the 26 holes used would be insufficient to determine the distribution of pressure…
NASA Technical Reports Server (NTRS)
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