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Wing design The design of a new airplane requires a gasoline tank of constant cross-sectional area in each wing. A scale draw- ing of a cross-section is shown here. The tank must hold 5000 lb of gasoline, which has a density of 42 lb/ft'. Estimate the length of the tank by Simpson's Rule. Yo Yi P2 |3 4 sY6 Yo = 1.5 ft, yı =1.6 ft, y2= 1.8 ft, y3=1.9 ft, Y4 = 2.0 ft, ys=Y6=2.1 ft Horizontal spacing = 1 ft

Wing design The design of a new airplane requires a gasoline tank of constant cross-sectional area in each wing. A scale draw- ing of a cross-section is shown here. The tank must hold 5000 lb of gasoline, which has a density of 42 lb/ft'. Estimate the length of the tank by Simpson's Rule. Yo Yi P2 |3 4 sY6 Yo = 1.5 ft, yı =1.6 ft, y2= 1.8 ft, y3=1.9 ft, Y4 = 2.0 ft, ys=Y6=2.1 ft Horizontal spacing = 1 ft

Mathematics For Machine Technology
Mathematics For Machine Technology
8th Edition
ISBN:9781337798310
Author:Peterson, John.
Publisher:Peterson, John.
Chapter61: Areas Of Circles, Sectors, And Segments
Section: Chapter Questions
Problem 50A
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Wing design The design of a new airplane requires a gasoline tank of constant cross-sectional area in each wing. A scale draw- ing of a cross-section is shown here. The tank must hold 5000 lb of gasoline, which has a density of 42 lb/ft'. Estimate the length of the tank by Simpson's Rule. Yo Yi P2 |3 4 sY6 Yo = 1.5 ft, yı =1.6 ft, y2= 1.8 ft, y3=1.9 ft, Y4 = 2.0 ft, ys=Y6=2.1 ft Horizontal spacing = 1 ft
Transcribed Image Text:Wing design The design of a new airplane requires a gasoline tank of constant cross-sectional area in each wing. A scale draw- ing of a cross-section is shown here. The tank must hold 5000 lb of gasoline, which has a density of 42 lb/ft'. Estimate the length of the tank by Simpson's Rule. Yo Yi P2 |3 4 sY6 Yo = 1.5 ft, yı =1.6 ft, y2= 1.8 ft, y3=1.9 ft, Y4 = 2.0 ft, ys=Y6=2.1 ft Horizontal spacing = 1 ft
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