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5858797

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Originally posted by lianglinlin at 2010-11-11 11:18:48:
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sunyang1988(½ð±Ò+5):ÐÁ¿àÁË£¬ºÜÏêϸ 2010-11-11 14:27:45
5858797(½ð±Ò+2): 2010-11-12 12:21:01
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Originally posted by 5858797 at 2010-11-11 10:30:09:
1.NOTE: Pressure and energy tail corrections will be added to all subsequent energy evaluations

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¡°The input data required by the static and dynamic methods consist of sets of coordinates of one or more configurations stored in archive (.arc) or history (.his) files.
In contrast, the input data required by the fluctuation formula option consist of cell parameters and stresses associated with frames in a trajectory. This information is always contained in history files and can also be saved in .tbl files using the Discover print table output option during dynamics. There is currently no way to generate .tbl files from the GUI. This must be done by adding BTCL commands to the .inp file for Discover. When many frames must be analyzed (say 1000-10000), the table file option is usually the only practical choice, since the resulting files are significantly more compact than history files (which will contain unwanted coordinate, velocity, and other information for all atoms). Table files should be set up to record instantaneous values (see Types of structures analyzed for further details).¡°
¼ÆËãElastic Constants¹ý³ÌÈçÏ£¬ÔÚDiscoverÖвÉÓÃÁË13¸öÓÅ»¯²½Ö裬1¸öÓÅ»¯²½ÖèÊdzõʼ¾²Ì¬½á¹¹ÓÅ»¯£¬ÆäÓà12¸öÓÅ»¯Êǵ¯ÐÔ³£Êý¼ÆË㣬°üº¬ÁË3¸ö Tensor StressºÍ3¸öSHear Stress£¬³õʼÓÅ»¯¼ÆËãÒ»°ãÊÇ1000´Î£¬ºóÐøµÄÓ¦±ä¾§°ûÓÅ»¯²ÉÓÃÁËÀ­ÉìºÍѹËõÁ½ÖÖģʽ£¬·ù¶Èλ0.005Ö®¼ä¡£Èç¹ûÊÇStatic ¼ÆË㣬һ°ãÈÏΪ²ÄÁÏÊǸ÷ÏòͬÐÔ¼ÙÉè¡£
Elastic Properties (static) for 1 frameIf only a single frame is analyzed, the .out file contains the matrix of coefficients (in GPa), plus a summary of the Poisson's ratio and the various moduli (Young's, bulk, shear, and the two Lam¨¦ constants) calculated assuming the material to be isotropic.
Elastic Properties (static) for 2 or more framesIf more than a single configuration has been analyzed, the .out file contains averages and standard deviations for all the elastic constants. The output produced by the program will also include a .tbl file containing histograms of the moduli, plus a table specifying elastic constants for each frame analyzed.
If you wish to see the matrix coefficients for each frame, you will need to view the .tbl file with a text editor. The file consists of a header section which describes the columns of the following data section. The matrix coefficients can be found in columns 9 through 21. Column 9 gives the frame number and the subsequent columns are C11,C22,C33,C12, C21,C13,C31,C23,C32,C44,C55 and C66.
If you wish to see the matrix coefficients for each frame, you will need to view the .tbl file with a text editor. The file consists of a header section which describes the columns of the following data section. The matrix coefficients can be found in columns 9 through 21. Column 9 gives the frame number and the subsequent columns are C11,C22,C33,C12, C21,C13,C31,C23,C32,C44,C55 and C66.
For each configuration submitted for elastic constants calculation by the fluctuation approach, both Eq. 126 and Eq. 127 are applied to obtain stiffness coefficients using the strain-strain and stress-strain correlation methods, respectively. The .out file is similar to that produced by the static method above, except that it contains two sets of stiffness coefficients; one for each fluctuation formula. In addition, the various moduli computed assuming the material to be isotropic are again provided. Finally, in this case, relevant quantities which need to be examined graphically are those pertinent to convergence of each fluctuation formula. Consequently, the .tbl file generated by the analysis contains running averages of the appropriate quantities <¦Åi ¦Åk> and <¦Åi¦Åj> in the fluctuation formulas.
For each configuration submitted for analysis using the molecular dynamics method of estimating mechanical properties, a total of three loading experiments are performed, in which a uniaxial tensile stress is applied stepwise along the x, y, or z directions. For each loading direction, constant stress dynamics is performed as a series of up to 10 stages, each of duration 1 ps. At the end of each stage, values of the internal stress tensor and of the strain tensor are recorded. Before continuing on to the next stage, the applied (external) stress is incremented by a predefined amount (0.05 GPa, or 500 bar). An experiment for any given pulling direction stops when the strain in that direction exceeds 0.2, or when all 10 stages have been completed, whichever occurs first. When all three loading experiments are completed, the recorded stress-strain data are averaged for all three directions.
The Young's modulus and Poisson's ratio are computed using a least-squares fit to the averaged tensile stress vs. tensile strain, and to the (negative) average lateral strain vs. tensile strain. The .out file contains a summary of the average Young's modulus and Poisson's ratio, plus values of the bulk and shear moduli derived therefrom according to Eq. 122 through Eq. 125. In addition, a .tbl file is produced containing the averaged stress/strain and lateral strain/tensile strain plots. If more than a single configuration has been analyzed, the output represents averages over the logical trajectory, in addition to averages over loading directions.
Finally, it should be noted that if the structure analyzed according to the molecular dynamics approach was originally obtained from an .arc or .car file, then the results refer to a temperature of 298 K. Otherwise (for example, if the structure was obtained from a .his file), the results refer to the same temperature as the simulation that generated the .his file.

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Originally posted by 5858797 at 2010-11-11 10:30:09:
1.NOTE: Pressure and energy tail corrections will be added to all subsequent energy evaluations

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