NAME_________________________________ CLASS____________________ DATE____________
Materials needed:
Explanation:
Step
1.
Dimesions of Wing: |
Thickness of wing ________________ |
Area of wing ________________ |
Step 2.
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Use the data in the table to create a graph which plots lift against angle of attack. Use a red pencil for this data set.
Step 3.
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Step 4.
Now you are ready to plot the lift values for the model wing. Use a blue colored pencil and plot the values on the same graph as the one used to depict the lift for the computer-generated wing in Step 2.
How do the plots compare?
Can you account for any discrepancy between the two?
Present your findings in the form of a technical report.