ME8096 Question Bank Gas Dynamics and Jet Propulsion Regulation 2017 Anna University

ME8096 Question Bank Gas Dynamics and Jet Propulsion

ME8096 Question Bank Gas Dynamics and Jet Propulsion Regulation 2017 Anna University free download. Gas Dynamics and Jet Propulsion Question Bank ME8096 pdf free download.

Sample ME8096 Question Bank Gas Dynamics and Jet Propulsion

1. In Rayleigh flow what is the Mach number at which the
total enthalpy is maximum?
BTL-2 Understanding
2. How do you specify equivalent diameter for noncircular
cross section?
BTL-2 Understanding
3. Give two practical examples for Fanno flow and Rayleigh
flow analysis.
ME8096 Question Bank Gas Dynamics and Jet Propulsion
4. Sketch the Rayleigh line on the T-s plane and explain the
significance of it.
BTL-3 Applying
5. In Rayleigh flow what is the Mach number at which the
total enthalpy is maximum?
BTL-1 Remembering
6. List some flow properties. BTL-1 Remembering
7. Label the limiting Mach number in isothermal flow. ME8096 Question Bank Gas Dynamics and Jet Propulsion
8. State the assumptions made to derive the equations for
isothermal flow.
BTL-4 Analyzing
9. Explain at what conditions the assumption of Rayleigh
flow is not valid in a heat exchanger.
BTL-5 Evaluating
10. What is the value of Mach number of air at the maximum
point in Rayleigh heating process?
BTL-6 Creating
11. List the governing equations that are useful to describe
the Rayleigh flow.
ME8096 Question Bank Gas Dynamics and Jet Propulsion
12. Write down the ratio of velocities between any two
sections in terms of their Mach number in a Fanno flow.
BTL-1 Remembering
13. Define Rayleigh line and state its application. BTL-1 Remembering
14. Define critical condition in Fanno flow. BTL-1 Remembering
15. State the assumptions made for Isothermal flow.

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