03545cam a2200517Ii 4500102892707MiAaHDL20250726000000.0m d cr bn ---auaua090624e196812 ohua bt f000 0 eng d(MiU)99187625982106381sdr-miu.99187625982106381(OCoLC)407125960(GWLA)gwla ocn407125960LHLengrdaLHLLHLOCLCFOCLCOOCLCQOCLCOTRAALMAIND 301.45/46-2:66-207/Volume VIAD 0683262AFFDL TR 66-207/V.6Cogan, J. P.,Jr.,author.FORMAT :Fortran matrix abstraction technique.Volume 6.Description of digital computer program - Phase 1 /J.P. Cogan, R. C. Morris, J. E. Serpanos, J. R. Wells.Wright-Patterson Air Force Base, Ohio :Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force,1968.viii, 735 pages :illustrations, figures, tables ;28 cm.texttxtrdacontentunmediatednrdamediavolumencrdacarrierAir Force Flight Dynamics Laboratory (U.S.). Technical report ;AFFDL TR 66-207/Volume VIResearch supported by the Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, and performed by the McDonnell Douglas Corporation, Douglas Aircraft Division.AD0683262 (from http://www.dtic.mil)."December 1968."Includes bibliographical references (page 735).FORMAT (FORtran Matrix Abstraction Technique) is a digital computer system consisting of three distint programs written entirely in Fortran IV. The system provides for generating, manipulating, printing, and plotting of large order (i.e., 2000) matrices commonly used in state-of-the-art structural analysis techniques. The capability of maintaining and automatic editing of case data has also been provided. Phase 1 of the system automatically generates matrices for joining, symmetric/antisymmetric disconnect, vibration, and stability analyses. Modules for converting continuous-to-discrete loads, analytic-to-discrete geometry, and a master case data file editor are provided to reduce input data requirements. Phase 2 of the system provides for the manipulation of matrices. The matrix operations (e.g., add, multiply, etc.), several special matrix operations, (e.g., adjoin), and severl control operations (e.g., save matrices, conditional IF test, etc.). Phases 3 of the system provides for self-explanatory report form printing of matrices and a nominal graphical display capability, including a geometric display.Air Force Contract No.F33615-67-C-1258, Project No. 1467, Task No. 146705.Mode of access: Internet.Strains and stresses.Airframes.Matrices.FORTRAN (Computer program language)Computer programs.Wells, J. R.,author.Serpanos, J. E.,author.Morris, R. C.,author.Air Force Flight Dynamics Laboratory (U.S.),issuing body.Air Force Wright Aeronautical Laboratories,sponsor.Douglas Aircraft Company.Aircraft Division,sponsor.Technical Report Archive & Image Library (TRAIL)3901510495673810289270720220802102022.020250726000000.020260227140654.02026-02-28T06:11:32Z2024-08-06T17:30:02ZSDR-MIUmiuALMAprepare.pl-004-009BKsdr-miu.99187625982106381MiUSDRGWLAmdp.39015104956738MIU99187625982106381MIUGWLA20260228googlemdp.390151049567381968pdbibUS fed doc