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We now have some idea about what models are available to simulate the flow over an aerofoil, and
also how to use the Hanley package to apply these methods. Keep referring to your model chart to
remind yourself about the limitations of different models.
Go back and reread section 2.5 and figure out the difference between the Navier-Stokes equations
and the Euler equations (i.e. what are the forces that are neglected in the Euler equations).
Before the laboratory session do some preparation by reading the following sections in Anderson:
Next week we will look to the assumptions for potential flow in detail. Now we want to start
investigating how aerofoil geometry and the aerodynamic forces and moments are related. This is the
fundamental question a designer asks. We also need to ask ourselves some questions about the
potential flow option, which is our main tool for the aerodynamic investigation.
Diffuser action: The flare, which increases the area of the duct, is known as a diffuser and its shape determines the rate of compression and the amount by which the air is com
In a CDMA system, the signal is spread over a large bandwidth by multiplying the transmitted symbol by a sequence of short pulses, also called chips. The
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Thin-skinned Structures The SCB geometry can't be used because the skins are too flexible. Instead, a centre-notch flexure (CNF) test can be used. A hole is drilled abo
FIRING ORDER If in multi cylinder engines, various cylinders are made to fire one after the other, interference between adjacent cylinders would occur, since these may have o
''If a non-coplaner force system is acted upon by equal and opposite forces,it must be in equilibrium''.State this statement is true or false.Please,give me a reason.
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Illustrate flat plate collectors. Describe liquid flat plate collector with relevant diagram.
I would like to ask in detail. How can I attach the files?
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