Unformatted text preview: use. Hand in hard copy of your use of fzero and list the value of upstream Mach number that you found. 2. Check your work using the nearest value to your answer to part 1 in the Normal Shock Table. This is appendix B in your text or can be downloaded from the `Educational Supplements ’ folder on the BlackBoard site. Is your work in part 1 correct?...
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- Fall '09
- Fluid Dynamics, Mach number, Shock wave, Scramjet, Supersonic, Ramjet