What other factor causes drag on the wing

Reference no: EM131467059

Question: A simple wing may be modeled as a 0.3 m wide flat plate set at an angle of 3° to an airflow at a Mach number of 2.5, the pressure in this flow being 40 kPa. Assuming that the flow over the wing is two-dimensional, estimate the lift and drag force per meter span due to the wave formation on the wing. What other factor causes drag on the wing?

Reference no: EM131467059

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