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An aircraft model tested in a wind tunnel produced 5 pounds of lift, giving a lift coefficient of 0.7. When the actual aircraft with a wing area of 650 ft^2 is in steady, level flight at altitude and the same angle of attack as the wind tunnel tests, the flight parameters are rho = 0.002 slug/ft3 and V_infinity = 400 ft/s.
a. How much does the actual aircraft weigh? Assume that the wind tunnel test conditions can be appropriately scaled to flight conditions (matched Mach number and Reynolds number, to be discussed later in the course).b. Describe the value of using dimensionless coefficients in this case.
Package Design Brief: Assume you are the packaging engineer for a large consumer products company. In this company, the Packaging Design Briefs are initiated by the marketing group and forwarded to the Package Engineering group.
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Wind turbines are becoming more and more common as a method of energy production, wind turbines by their very nature are dynamic and are subject to and create their own internal and external kinematics and kinetics.
8 x product engineering and design review (week 2 – 12), ~3 pages per item which must contain a brief description of the product then delve into concepts such as materials selection, manufacturing methods, life cycle analysis, recyclability and overa..
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