|
发表于 2009-2-24 21:49:53
|
显示全部楼层
你只需要复制“气动”数据,复制过头了,就是出现那些问题。
比如这些就是气动数据:
CLa=0.5341
CD0=0.0013
CDL=0.0015
Cmq=-0.2178
Cmad=0.0120
Cyb=-0.0209
Clb=-0.0908
Clp=-0.0661
Clr=0.0152
Cnb=-0.1555
Cnp=0.0020
Cnr=-0.0039
CLaMachTableNumData=4
CLaMachTableDeltaX=0.40
CLaMachTableStartX=0.00
CLaMachTableData=0.994,1.000,1.020,1.090
CD0MachTableNumData=4
CD0MachTableDeltaX=0.40
CD0MachTableStartX=0.00
CD0MachTableData=1.408,1.000,1.046,7.380
CDLAlphaTableNumData=15
CDLAlphaTableDeltaX=4.00
CDLAlphaTableStartX=-28.00
CDLAlphaTableData=49.000,36.000,25.000,16.000,9.000,4.000,1.000,0.000,1.000,4.000,9.000,16.000,25.000,36.000,49.000
CmqMachTableNumData=4
CmqMachTableDeltaX=0.40
CmqMachTableStartX=0.00
CmqMachTableData=0.866,1.000,1.918,-4.332
ClbAlphaTableNumData=15
ClbAlphaTableDeltaX=4.00
ClbAlphaTableStartX=-28.00
ClbAlphaTableData=-1.308,-1.020,-0.731,-0.443,-0.154,0.134,0.423,0.711,1.000,1.289,1.577,1.866,2.154,2.443,2.731
ClpAlphaTableNumData=15
ClpAlphaTableDeltaX=4.00
ClpAlphaTableStartX=-28.00
ClpAlphaTableData=1.816,1.595,1.408,1.255,1.136,1.051,1.000,0.983,1.000,1.051,1.136,1.255,1.408,1.595,1.816
ClrAlphaTableNumData=15
ClrAlphaTableDeltaX=4.00
ClrAlphaTableStartX=-28.00
ClrAlphaTableData=-7.000,-6.000,-5.000,-4.000,-3.000,-2.000,-1.000,0.000,1.000,2.000,3.000,4.000,5.000,6.000,7.000
CnpAlphaTableNumData=15
CnpAlphaTableDeltaX=4.00
CnpAlphaTableStartX=-28.00
CnpAlphaTableData=-16.629,-11.877,-8.294,-5.621,-3.641,-2.159,-1.000,0.000,1.000,2.159,3.641,5.621,8.294,11.877,16.629
CnrAlphaTableNumData=15
CnrAlphaTableDeltaX=4.00
CnrAlphaTableStartX=-28.00
CnrAlphaTableData=40.756,29.989,20.878,13.424,7.626,3.485,1.000,0.172,1.000,3.485,7.626,13.424,20.878,29.989,40.756
XacMachTableNumData=4
XacMachTableDeltaX=0.40
XacMachTableStartX=0.00
XacMachTableData=0.426,0.434,0.496,-0.048
CheckStall=TRUE
CLmax=0.1369
AlphaStall=13.86
AlphaMax=14.77
AlphaDepart=17.96
Ymac=-1.06 |
|