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NX Nastran DMAP Programmer's Guide - Kxcad.net

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634<br />

Chapter 3<br />

Name<br />

Chapter 2<br />

Name<br />

Description<br />

MESH Mesh type for aerodynamic or structural components:<br />

'AERO' or 'STRU'.<br />

MESTNL Nonlinear element summary table at current step.<br />

Output by NLITER and NLTRD2.<br />

MEW Modal effective weight matrix. Output by EFFMAS.<br />

MFACE Face table for p-element analysis. Output by GP0.<br />

MFHH Fluid partition of modal mass matrix MHH.<br />

MGG Mass or radiation matrix in g-size.<br />

MHH Generalized (modal) mass matrix<br />

MHH1 Modified generalized (modal) mass matrix. Output by<br />

FA1.<br />

MI Modal mass matrix. Output by READ and LANCZOS.<br />

Mi Matrix data block. Output by INPUTT4 and input to<br />

MATPRN and OUTPUT4.<br />

MIDLIS Table of pairs of user-supplied material property<br />

identification numbers (MIDs) and internal baseline<br />

MIDs. Output by DSABO.<br />

MKK Mass matrix in cyclic components. Output by CYCLIC3.<br />

MKLIST Table of Mach number and reduced frequency pairs.<br />

Output by GETMKL.<br />

MLAM Matrix relating element forces to source strengths.<br />

Output by MGEN.<br />

MLAM2 Secondary matrix relating element forces to source<br />

strengths. Output by MGEN.<br />

MLL Mass matrix reduced to the l-set.<br />

MLR Mass matrix partition (l-set by r-set) from MTT.<br />

MOA Mass matrix partition (o-set by a-set) from MFF.<br />

MOFPi Matrix form of the i-th output table. Output by DRMH1<br />

and DRMS1.<br />

MON Merged monitor table. Output by MRGMON.

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