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By Sarişin M.N.

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18000 16000 Altitude (m) 14000 12000 10000 8000 6000 4000 2000 0 0 50 100 150 200 Time (s) Figure 1-25. Flight Trajectory of Missile X. 5 1 0 50 100 150 200 250 300 Time (s) Figure 1-26. Mach Number Evolution of Missile X. Air Mass Flow Rate vs. Time 9 Air Mass Flow Rate (kg/s) 8 7 6 5 4 3 2 1 0 0 20 40 60 80 100 120 140 160 Time (s) Figure 1-27. Mass Flow Rate Captured by Inlets vs. Time 37 180 200 9 Static Pressure (Bar) 8 7 6 5 4 3 2 1 0 0 20 40 60 80 100 120 140 160 180 200 Time (s) Figure 1-28.

A tradeoff study is performed to choose the best configuration for the present case. The results of the study are given in Table 2-1. For four pressures alternative (50, 100, 150 and 200 bar), density and volume required to store 1650 kg of air are calculated. Table 2-1. 21 Pressure (bar) Case 1 to Case 4 is studied during the air tank design. 2. PRESSURE VESSEL DESIGN Case 1 to 4 given in Table 2-1 is studied in detail in this section. In the analysis, quenched/tempered alloy steel is used. Ultimate Tensile Strength of the material is 828 MPa.

Due to the extremely high temperatures produced by the arc, ionized species are created that react to form NOx and other undesired constituents that contaminate the air stream. The presence of these contaminants, and the fact that oxygen dissociation begins at approximately 2500K, sets the upper limits of combustion testing in arc facilities. Above this temperature, care must be taken to account for the chemical effects of the contaminants and dissociated species on combustion. The high power requirements of arc heaters make them very expensive to operate.

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