A light aircraft with a wing area of 200 ft2 and a weight of 2000 lbf has a lift coefficient of 0.40 and a drag coefficient of 0.05. Determine the power (in horsepower) required to maintain level flight.

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The purpose of a lab is to do your "expirements" the importance of the topic is so you can now what the story is about and the last one is because no one is me with my question ( what is 3 over 4 x - 9 = 27 maybe you can )

Multiply the 3 dimensions, assuming it is a rectangular cuboid, to get the volume in cm³ divide mass by volume to get density in g/cm³