79 



pressure was varied l).v the use of the upper valve, throttling the up- 

 stream section. In this way up-stream pressures of from 40 pounds per 

 square inch down hy 5 Ave pounds per square inch steps to the lower 

 limit were effected. The apparatus discharged into a weighing tank and 

 the discharge was weighed. The temperature of the water was taken 

 every minute because this temperature varied greatly throughout the tests, 

 due to the fact that the standpipe tank was connected to the condenser 

 of a Corliss engine. (With respect to the effect of the temperature on the 

 results, it may be said that when the temperature of the discharge rose 

 above the 100° F., the tail pressure gauge showed a very unsteady pres- 

 sure, the needle vibrating with a range of as much as one-half pound. 

 The disc was no doubt at this time subject to vibrations, -which, when 

 the temperature of the water rose to 110° F., were of such frequency as 

 to cause a musical note. Under the latter condition the needle was too 

 sluggish to respond and remained at a fixed position. The movement is 

 probably connected with alternate periods of vaporization and condensia- 

 tion of the water on the upper side of the disc.) 



Results.— The following combinations of nozzle and disc were used: 

 One-eighth-iuch nozzle. 1-inch disc; %-inch nozzle, li/o-inch disc; %-inch 

 nozzle, 2-inch disc; 3-16-inch nozzle, 1-inch disc; 3-16-inch nozzle, l^^-inch 

 disc; 3-16-inch nozzle. 2-inch disc; 14-inch nozzle, 1-inch disc; i/4-inch noz- 

 zle, li/o-inch disc; i/4-inch nozzle, 2-inch disc. 



Of these, the i^-inch nozzle gave successful results; the %-inch nozzle, 

 with the 2-inch disc, gave the best results. These are shown in Fig. 4. 

 In working the head pressure down toward the tail pressure the former 

 would approach a critical point at which the difference of pressure became 

 so slight that the regulating effect ceased and both head and fail gauges 

 suddenly moved to the same reading. The disc at this period, no doubt, 

 dropped away from the jet. That is a certain difference of pressures is 

 needed to enable the apparatus to work. This difference of pressure be- 

 came greater as the tail pressure was increased, as is shown in Fig. 4. 



In experiments with the other orifices mentioned the lines shown in 

 Fig. 4 became straight lines inclined to the horizontal. The hump in Fig. 4 

 was characterized by an unsteady head pressure. 



One disc was bevelled so as to give a constant area of passageway to 

 the expanding ring of watei", that is, it was dished with the deepest 

 part next to the nozzle. This disc preserved a constant difference of pres- 

 sure between the head and tail pressures. 



