Solar Cells: Operating Principles, Technology, and System by Martin A. Green
By Martin A. Green
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Additional resources for Solar Cells: Operating Principles, Technology, and System Applications (Prentice-Hall series in solid state physical electronics)
Equations (1-116) and (1-117) each represent a curve in the h-s diagram (which is a function of Eqs. (1-6) and (1-52». The former is called the Rayleigh line and the latter the Fanno line. These lines intersect at two points, whose coordinates satisfy both equations and, therefore, correspond to the state of the flow on opposite sides of the shock. Figure 1-1 shows typical forms of these two curves. The Rayleigh and Fanno lines are plotted as follows. When conditions on the upstream side of the shock are given, the constants C L C2, and C3 can be computed.
Curve f indicates that the static pressure across the shock decreases and the Mach number which is supersonic at the left of the shock decreases and becomes subsonic at the right of the shock. Since after the shock Mach number is less than 1, the velocity decreases and static pressure increases in the divergent section behind the shock which is in contrast to the divergent section in front of the shock, where the Mach number increases continuously 42 Jet, Rocket, Nuclear, Ion and Electric Propulsion from unity at the throat to a supersonic Mach number MI.
1-13c), it gives poor diffusion efficiency. Figure I-lad shows the farthest upstream position (at the throat section) for which the flow is still stable. However, a slight disturbance in the flow pattern of Fig. 1-13d will move the shock out of the inlet. Such a diffuser possesses the so-called hysteresis effect. During acceleration, the shock will not be swallowed until the speed Md (Fig. 1-12) is reached. Once swallowed, the shock will not be pushed out upon deceleration until the speed Mb (Point b of Fig.