A blade of the main rotor of a hovering helicopter is subjected to the y direction distributed forces shown, where values are known at points A, B, and C. Determine the constants a, b, and c so that the quadratic polynomial, ax2 + bx + c, describes this loading. Using this polynomial, determine the total force produced by this distribution and the x position of its line of action.Use Simpson’s rule to find the x-position of the line of action, then solve for the total force wc = 6kN/mWB = 4 kN/mWA = 1 kN/m3 m²-3 m²0.4mZA blade of the main rotor of a hovering helicopter is subjected to the y directiondistributed forces shown, where values are known at points A, B, and C. Determine theconstants a, b, and c so that the quadratic polynomial, ax2 + bx + c, describes thisloading. Using this polynomial, determine the total force produced by this distributionand the x position of its line of action.Use Simpson's rule to find the x-position of the line of action, then solve for the totalforce

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wc = 6kN/m WB = 4 kN/m x WA = 1 kN/m 3 m -3 m² -0.4m Z A blade of the main rotor of a hovering helicopter is subjected to the y direction distributed forces shown, where values are known at points A, B, and C. Determine the constants a, b, and c so that the quadratic polynomial, ax2 + bx + c, describes this loading. Using this polynomial, determine the total force produced by this distribution and the x position of its line of action. Use Simpson's rule to find the x-position of the line of action, then solve for the total force

wc = 6kN/m WB = 4 kN/m x WA = 1 kN/m 3 m -3 m² -0.4m Z A blade of the main rotor of a hovering helicopter is subjected to the y direction distributed forces shown, where values are known at points A, B, and C. Determine the constants a, b, and c so that the quadratic polynomial, ax2 + bx + c, describes this loading. Using this polynomial, determine the total force produced by this distribution and the x position of its line of action. Use Simpson's rule to find the x-position of the line of action, then solve for the total force

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter4: Numerical Analysis Of Heat Conduction

Section: Chapter Questions

Problem 4.17P

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