Estimates with Numerical DataWing design The design of a
Chapter 8, Problem 25E(choose chapter or problem)
Problem 25E
Estimates with Numerical Data
Wing design The design of a new airplane requires a gasoline tank of constant cross-sectional area in each wing. A scale drawing of a cross-section is shown here. The tank must hold 5000 lb of gasoline, which has a density of 42 lb/ft3 .Estimate the length of the tank by Simpson’s Rule.
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