An airplane wing, with chordlength of 5 ft and span of 30 ft. is designed to fly in standard air at a speed of 230 ft/sec. A 1/10 scale model of this wing is to be tested in a water tunnel. What flow speed is necessary in the water tunnel to achieve dynamic similarity? What will theratio of drag forces measured in the model flow to those on the prototype wing be? Ignore compressibility

answer:

design model: consists of design geometry; can be 2d or 3d; typically has a black background.

design files: drawing created with microsoft expression design, a drawing and design program for windows; may contain both vector and raster graphics; can also include multiple layers and various image effects.

elements: an element is a single part of a larger group.

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A Carnot heat engine receives heat from a reservoir at 900$^\circ{}$C at a rate of 800 kJ/min and rejects the waste heat to the ambient air at 27$^\circ{}$C. The entire work output of the heat engine is used to drive a refrigerator that removes heat from the refrigerated space at -5$^\circ{}$C and transfers it to the same ambient air at 27$^\circ{}$C. Determine (a) the maximum rate of heat removal from the refrigerated space and (b) the total rate of heat rejection to the ambient air. Answers: (a) 4982 kJ/min, (b) 5782 kJ/min