We have made a first study of the calorimetric response to 10 GeV/c charged pions in the transition region between barrel and endcap for the scintillator-tile design pursued at Argonne National Laboratory using the simulation program ANLSIM. For (very nearly) projective tower orientations in the barrel, the crack appears deep within a narrow angular range, causing a loss of the response in that region up to 40%. Pointing the towers onto the beam axis 35 cm or more away from the nominal-interaction point leads to a shortened depth of the barrel-endcap crack as seen by particles incident from the interaction region, cutting the maximum loss down by almost one half. The worsening of the resolution follows the same trend. Introduction of a solenoidal coil in front of the calorimeter causes an overall degradation of the response by an amount nearly comparable to the effect of the crack. Electrons of the same incident momentum are more strongly affected by the coil than pions but see only a much narrower region of degradation by the crack. 15 refs., 6 figs., 2 tabs.

An examination of a coherency criteria for high velocity jets is discussed in this paper. An analysis of the classical Pugh, Eichelberger, Rostoker jetting theory is used to develop an equation that defines the maximum coherent jet velocity as a function of the liner material sound speed, the liner beta angle, and the magnitude direction of the liner collapse velocity vector. The liner material sound speed is assumed to be the liner material shock velocity at the time of liner material collapse. This shock velocity is a function of the collapse pressure in the stagnation region and thus varies with time and position along the liner. The analysis indicates that coherent jets at velocities greater than three times the liner shock velocity are possible with some combinations of the beta and collapse vector angles while incoherent jets at velocities equal to two times the liner shock velocity could occur with other combinations. The objectives of this paper are to examine the theory used to calculate jet velocity and to develop a criteria for calculating the maximum coherent jet tip velocity. 13 refs., 6 figs.

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