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A cross-section of an airplane wing is shown. Measurements of the thickness of the wing, in centimeters, at 20-centimeter intervals are 6.2, 20.3, 26.2, 28.5, 27.6, 27.1, 23.6, 20.5, 15.2, 8.6, and 3.5. Use the Midpoint Rule to estimate the area of the wing's cross-section. O2100 cm² O4200 cm² O4092 cm² O 3952 cm² O 3844 cm² O 4146 cm² -200 cm

A cross-section of an airplane wing is shown. Measurements of the thickness of the wing, in centimeters, at 20-centimeter intervals are 6.2, 20.3, 26.2, 28.5, 27.6, 27.1, 23.6, 20.5, 15.2, 8.6, and 3.5. Use the Midpoint Rule to estimate the area of the wing's cross-section. O2100 cm² O4200 cm² O4092 cm² O 3952 cm² O 3844 cm² O 4146 cm² -200 cm

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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A cross-section of an airplane wing is shown. Measurements of the thickness of the wing, in centimeters, at 20-centimeter intervals are 6.2, 20.3, 26.2, 28.5, 27.6, 27.1, 23.6, 20.5, 15.2, 8.6, and 3.5. Use the Midpoint Rule to estimate the area of the wing's cross-section. O 2100 cm² O 4200 cm² O4092 cm² O 3952 cm² O3844 cm² O 4146 cm² -200 cm
Transcribed Image Text:A cross-section of an airplane wing is shown. Measurements of the thickness of the wing, in centimeters, at 20-centimeter intervals are 6.2, 20.3, 26.2, 28.5, 27.6, 27.1, 23.6, 20.5, 15.2, 8.6, and 3.5. Use the Midpoint Rule to estimate the area of the wing's cross-section. O 2100 cm² O 4200 cm² O4092 cm² O 3952 cm² O3844 cm² O 4146 cm² -200 cm
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