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Derive an analogous relation for V””” for a propeller-driven airplane in terms of the power-to-weight ratio (power loading).

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Using your result from Prob. 6.35, calculate the maximum velocity of the CP-1 at sea level, and compare your result with the numerical solution in Sec. 6.6. Prob. 6.35 Examine Eq. (6.44) in the text. This equation is an explicit relation for V””” in terms of the thrust-to-weight ratio for the airplane, and hence allows a quick analytical calculation of V””” for jet-propelled airplanes. Derive an analogous relation for V””” for a propeller-driven airplane in terms of the power-to-weight ratio (power loading). Note: You will find a relation that relates power loading and V “””’ but you will also discover that it is not possible to solve this relation explicitly for V =· Even so, this relation still allows a quicker solution for V””” for propeller driven airplanes in comparison to the numerical solution discussed in Sec. 6.6.

 
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