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操作系统是centos6.5,前面运行的好好的,问题出现在最后5行:
Enter NACA 4 or 5-digit airfoil designation i> 0012
Max thickness = 0.120032 at x = 0.297
Max camber = -0.000000 at x = 0.015
Buffer airfoil set using 245 points
Blunt trailing edge. Gap = 0.00252
Paneling parameters used...
Number of panel nodes 160
Panel bunching parameter 1.000
TE/LE panel density ratio 0.150
Refined-area/LE panel density ratio 0.200
Top side refined area x/c limits 1.000 1.000
Bottom side refined area x/c limits 1.000 1.000
XFOIL c> GDES
You are working with the buffer airfoil
X Error of failed request: BadValue (integer parameter out of range for operation)
Major opcode of failed request: 1 (X_CreateWindow)
Value in failed request: 0x0
Serial number of failed request: 8
Current serial number in output stream: 13
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