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Unformatted text preview: Name: _____________ ___________ 2 6. Write down the integral form of conservation of momentum for an Eulerian Method of Description for a fixed control volume. Please describe each of the terms. 7. When is flow in a boundary layer considered to be irrotational? 8. What is required for a flow to be isentropic? 9. What is required for a thermally and calorically perfect gas? 10. Which causes the greatest loss in stagnation pressure? A. A normal shock in a Mach 2 flow B. An oblique shock in a Mach 2 flow C. A Prandtl-Meyer expansion in a Mach 2 flow D. A Mach Wave in a Mach 2 flow...
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This note was uploaded on 09/05/2011 for the course EAS 4101 taught by Professor Sheplak during the Spring '08 term at University of Florida.
- Spring '08