ME 471 - Quiz Solutions

Refer figure 117 from the textbook 3 for an angle of

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Unformatted text preview: er Figure 1.17 from the textbook. 3. For an angle of attack of , calculate the lift and drag coefficients aerofoil having normal and axial force coefficients as and Refer Equation 1.18 and 1.19 from the textbook. and . of an ME 471.3 Introduction to Aerodynamics Department of Mechanical Engineering Winter 2014 Instructor – Rajat Chakravarty Quiz 2 Instructions: Write all solutions on this page itself. No additional paper will be provided. 1. An airfoil has a center of pressure at a distance of from the leading with respective coefficients and . Calcu...
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