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Next: Small Perturbation Solution Up: Operating Equations and Analysis Previous: Operating Equations and Analysis Index The Limitations of the Shock WaveWhen the upstream Mach number becomes very large, the downstream Mach number (see equation (5.22)) is limited by This result is shown in Figure (5.3). The limits of the pressure ratio can be obtained by looking at equation (5.16) and by utilizing the limit that was obtained in equation (5.38).
Next: Small Perturbation Solution Up: Operating Equations and Analysis Previous: Operating Equations and Analysis Index Created by:Genick Bar-Meir, Ph.D. On: 2007-11-21 |