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available to download on your DASHBOARD and a copy sent to your email address
Question Details
| Item Name | Price |
|---|---|
| Expert Answer #770539 The NACA 4412 airfoil has a mean camber line given by \[ \frac{z}{c}=\left\{\begin{array}{ll} 0.25\ ... | $5 |
| TOTAL | $5 |
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