A Program for Calculating Load Coefficient Matrices Utilizing the Force Summation Method, L218 (LOADS). Volume 1: Engineering and Usage, Volume 1

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National Aeronautics and Space Administration, 1979 - 143 pages

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Contents

1
1
PROGRAM STRUCTURE AND DESCRIPTION
18
Flow of L218 Card Input Data
28

6 other sections not shown

Common terms and phrases

A10 Keyword acceleration Aero aerodynamic force aerodynamic panel ANGLES AREA axis system blank bodies Boeing Commercial Airplane calculate CALLED Card Input Card set Card Set 4.0 COLS column COORD coordinate Default defined DESCRIPTION Keyword diagonal direction DISK displacement DLOAD dummy load dummy nodes equations ERROR IN READING factor FATAL ERROR Figure FORMAT DESCRIPTION 1-10 FREQUENCY FULL VERT gust IINODE included increase inertia data Input Data interpolation introducing J-MATRIX Keyword indicating load coefficient matrices load set mass mass matrix MASSTP matrix means method Modal mode moments Name necessary NMODES node numbers Note NPLDS NPTAP Omit Optional output overlay panel loads PLDS RAVD Repeat card RGEN rotation SATAP SCALED SCALR2 selected shears structural nodes Subroutine Diagnostics surface SURFACE CARD SURFACE NODE surface number Table TAPE transformation Type VARIABLE FORMAT DESCRIPTION VBMT XMASS

Bibliographic information

TitleA Program for Calculating Load Coefficient Matrices Utilizing the Force Summation Method, L218 (LOADS). Volume 1: Engineering and Usage, Volume 1
Volume 2853 of NASA contractor report
AuthorR. D. Miller
PublisherNational Aeronautics and Space Administration, 1979
Original fromNational Aeronautics and Space Administration (NASA)
DigitizedJun 8, 2010
Length143 pages
  
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