4.18 A flat plate is immersed in a Mach 2 flow at standard sea level conditions at an angle of attack of 2°. Assuming the same shear stress distribution given in Example 1.8, calculate, per unit span: (a) lift, (b) wave drag, and (c) skin friction drag. What percentage of the total drag is skin-friction drag? Compare this percentage with the 10° angle of attack case discussed in Example 1.8.

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Chapter5: Analysis Of Convection Heat Transfer
Section: Chapter Questions
Problem 5.29P: Air at 20C flows at 1 m/s between two parallel flat plates spaced 5 cm apart. Estimate the distance...
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4.18 A flat plate is immersed in a Mach 2 flow at standard sea level conditions at
an angle of attack of 2°. Assuming the same shear stress distribution given
in Example 1.8, calculate, per unit span: (a) lift, (b) wave drag, and (c) skin
friction drag. What percentage of the total drag is skin-friction drag? Compare
this percentage with the 10° angle of attack case discussed in Example 1.8.
Transcribed Image Text:4.18 A flat plate is immersed in a Mach 2 flow at standard sea level conditions at an angle of attack of 2°. Assuming the same shear stress distribution given in Example 1.8, calculate, per unit span: (a) lift, (b) wave drag, and (c) skin friction drag. What percentage of the total drag is skin-friction drag? Compare this percentage with the 10° angle of attack case discussed in Example 1.8.
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