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The fuel tanks for airplanes are in the wings, cross section below. The tank must hold 5800 lb of fuel wi density 42 lb/ft³. Estimate the length of the tank using Simpson's Rule. yo 31 32 33 34 35 36 Horizontal spacing= 1.6 ft Yo=1.4 ft, y₁ = 1.6 ft, y₂ = 1.7 ft, y3 =2 ft, y₁=2.2 ft, Y5 = 2.3 ft, y = 2.2 ft The length of the tank is ft.

The fuel tanks for airplanes are in the wings, cross section below. The tank must hold 5800 lb of fuel wi density 42 lb/ft³. Estimate the length of the tank using Simpson's Rule. yo 31 32 33 34 35 36 Horizontal spacing= 1.6 ft Yo=1.4 ft, y₁ = 1.6 ft, y₂ = 1.7 ft, y3 =2 ft, y₁=2.2 ft, Y5 = 2.3 ft, y = 2.2 ft The length of the tank is ft.

Advanced Engineering Mathematics
Advanced Engineering Mathematics
10th Edition
ISBN:9780470458365
Author:Erwin Kreyszig
Publisher:Erwin Kreyszig
Chapter2: Second-order Linear Odes
Section: Chapter Questions
Problem 1RQ
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The fuel tanks for airplanes are in the wings, cross section below. The tank must hold 5800 lb of fuel with density 42 lb/ft³. Estimate the length of the tank using Simpson's Rule. yo 31 32 33 34 35 36 Horizontal spacing = 1.6 ft Yo=1.4 ft, y₁ = 1.6 ft, y₂ = 1.7 ft, y3 =2 ft, y4 = 2.2 ft, Y5 = 2.3 ft, Y₁ = 2.2 ft The length of the tank is ft. (Round to the nearest tenth as needed.)
Transcribed Image Text:The fuel tanks for airplanes are in the wings, cross section below. The tank must hold 5800 lb of fuel with density 42 lb/ft³. Estimate the length of the tank using Simpson's Rule. yo 31 32 33 34 35 36 Horizontal spacing = 1.6 ft Yo=1.4 ft, y₁ = 1.6 ft, y₂ = 1.7 ft, y3 =2 ft, y4 = 2.2 ft, Y5 = 2.3 ft, Y₁ = 2.2 ft The length of the tank is ft. (Round to the nearest tenth as needed.)
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