For the sine-wave airfoil shape of Prob. 9.154, with Ma∞ = 2.5, k = 1.4, t/C =

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For the sine-wave airfoil shape of Prob. 9.154, with Ma∞ = 2.5, k = 1.4, t/C = 0.1, and α = 0°, plot (without computing the overall forces) the pressure distribution p(x)/p∞ along the upper surface for
(a) Ackeret theory and
(b) An oblique shock plus a continuous Prandtl-Meyer expansion.

For the sine-wave airfoil shape of Prob. 9.154 Distribution
The word "distribution" has several meanings in the financial world, most of them pertaining to the payment of assets from a fund, account, or individual security to an investor or beneficiary. Retirement account distributions are among the most...
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