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SaveTarget ( FileName ) |
Design Card |
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| Arguments | FileName | the fully qualified name of the file to write, enclosed in double quotes |
| Description | Writes the target pressure distribution to the specified file. | |
| Remarks | The output file contains the
pressure coefficient at each coordinate point of airfoil and the design
angle of attack. The file can be read back using the
LoadTarget() command. You must initialize the design before using this command either by using the Init() method or by reading a target Cp distribution from a file. |
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