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Save ( FileName[, OutputVariable] ) |
Velocity Card |
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| Arguments | FileName | the fully qualified name of the file to write, enclosed in double quotes |
| OutputVariable | Optional, A number which indicates the variable to export (0=v/V, 1=Cp, 2=Mach). | |
| Description | Writes the airfoil geometry and the velocity distributions as created by a previous analysis to the specified file. | |
| Remarks | The output file contains the
distributions in the same format as it is used by the "CopyText" command. You must execute an Analyze() command to set the required parameters like angle of attack range before using this command. Depending on the variable used by the Analyze command (v/V, Cp, Mach) the output contains the corresponding values. Performs the same action as the "Save..." button. |
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