Aerodynamics Q&A

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Aerodynamics

Question 1

The continuity equation deals with the law of conservation of mass. The law of conservation of mass is illustrated by the continuity equation based on two aspects. Firstly, the air flow may either be steady or unsteady.

For the unsteady flow,

The second aspect of the equation deals with a steady flow and it’s illustrated as

Applying this is an aircraft’s engine an aircraft requires the correct amount of airflow in order to increase its thrust in flight. Since at cruise speed an engine thrust accounts for only 17 %, there is need for the aircraft to take in more air in order to increase the thrust. The continuity equation is therefore an important contribution to the airflow into and out of the engine. The pressure has thus to be balanced at the compressor in order to allow for increased intake at the intake. This would then be as stipulated by the continuity equation which illustrate that the mass flow rate of change at the intake minus the mass flow rate at the outlet will give the rate of change of mass storage. This storage mass is what influence the increased thrust.

There is also a very large contribution of the airflow intake to the pressure ratio of the plane. This means that since the engine’s effect to the pressure is negligible, it’s the air flow which affects the pressure ratio. For this reason, the amount of air being sucked in by the plane determines the pressure ration as well as the thrust. There is therefore a need for increased air intake in order to influence the rate of change of storage.

In order for the aircraft to experience more air intake, several parameters have to be altered. This is because the air intake into an aircraft is influenced by flow distortion, turbulence ...

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...principles that are related to the gas laws and the thermodynamic principles. For this reason, these aspects are very important since they illustrate the various changes in pressure, volume, and temperature. A change in any of the three elements cause significant change to the others as well as in the energy generated during the entire time. The thermodynamic principles help in the explanation of the energy differences as well as entropy generated from the initial internal energy in systems.

Works Cited

Charles Edward D and James E. Lewis. Flight theory and aerodynamics: a practical guide for operational safety. New York, NY: Wiley-IEEE, 2000. Print.

Glen Research Center. Ideal Brayton Cycle. Glen Research Center, 2011. Web. 16 May. 2011.

Roskam Jan and Chuan-Tau Edward Lan. Airplane aerodynamics and performance. Lawrence, KS: DAR Corporation, 1997. Print.

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