Find the following based on the graphs given (angle of attack: 6 degrees, Re: 3.01*10^6, chord length: 0.75m, velocity: 60 m/s, standard atmosphere): Lift coefficient, c₁, moment coefficient at the ¼ chord point, Cm,c/4, and the drag coefficient, ca.d. Lift per unit span, L', drag per unit span, D', and moment about the 14 chord point per unit span, M'c/4-C. Cmc/4NOTE: Use theoutermost scalefor the momentcoefficient.47812Moment coefficient, C7ပြီး ယခင်GSection lift coefficient, c3.63.22.82.42.01.61.2-1.2-1.6-2.0THEORY OF WING SECTIONS-80816Section andle of attackx (deg)NACA 2412 Wing Section-162432y/c| J024020Section drog coefficient, caCaD168.0125.008D0402-14.2APPENDIX IVx/c6ReO 3.1 x 1065.7 x 106◊ 8.9 x 106A 5.7 x 106-8.81.0a.c. position036032028x/cy/c.239.006.243-.004.247-.018Standard roughnessSection lift coefficient, ₁NACA 2412 Wing Section (Continued)81.24791.6

Name: Find the following based on the graphs given (angle of attack: 6 degre
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Description: Find the following based on the graphs given (angle of attack: 6 degrees, Re: 3.01*10^6, chord length: 0.75m, velocity: 60 m/s, standard atmosphere): Lift coefficient, c₁, moment coefficient at the ¼ chord point, Cm,c/4, and the drag coefficient, ca.

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Answered: Find the following based on the graphs…

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Mechanical Engineering

Find the following based on the graphs given (angle of attack: 6 degrees, Re: 3.01*10^6, chord length: 0.75m, velocity: 60 m/s, standard atmosphere):

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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