| LDR | 02967cam a2200481Ii 4500 | ||
| 001 | 102893803 | ||
| 003 | MiAaHDL | ||
| 005 | 20230928000000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 090624e196812 ohua bt f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡a(MiU)99187625981806381 |
| 035 | ⊔ | ⊔ | ‡asdr-miu.99187625981806381 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)407170401 |
| 035 | ⊔ | ⊔ | ‡a(GWLA)gwla ocn407170401 |
| 040 | ⊔ | ⊔ | ‡aLHL ‡beng ‡erda ‡cLHL ‡dOCLCF ‡dOCLCO ‡dOCLCQ ‡dOCLCO ‡dTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/46-2:66-207/Volume VII/Supplement I |
| 088 | ⊔ | ⊔ | ‡aAD 0713840 |
| 088 | ⊔ | ⊔ | ‡aAFFDL TR 66-207/V.7/SUPP.I |
| 100 | 1 | ⊔ | ‡aFrank, J. A., ‡eauthor. |
| 245 | 1 | 0 | ‡aFORMAT : ‡bFortran matrix abstraction technique. ‡nVolume 7 - Supplement 1. ‡pDescription of digital computer program - Phase 3 - Extended / ‡cJ.A. Frank. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, ‡c1968. |
| 300 | ⊔ | ⊔ | ‡av, 38 pages : ‡billustrations, figures ; ‡c28 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.). Technical report ; ‡vAFFDL TR 66-207/Volume VII/Supplement I |
| 500 | ⊔ | ⊔ | ‡aResearch supported by the Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, and performed by the Douglas Aircraft Company. |
| 500 | ⊔ | ⊔ | ‡aAD0713840 (from http://www.dtic.mil). |
| 500 | ⊔ | ⊔ | ‡a"August 1970." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (pages 37-38). |
| 520 | ⊔ | ⊔ | ‡aThe FORMAT System has been updated by the incorporation of additional basic capability and the refinement of existing capability. A simpler mode of updating case data and extended force method matrix generation capability has been incorporated in Phase I of the system. A refined 'Structure Cutter' module, capabilities for matrix partitioning and instruction looping, and an additional eigenvalue/eigenvector extraction module have been incorporated in Phase II. Finally the limitations which existed in the matrix plotting capability in Phase III have been eliminated. Programming documentation for the extended capability of Phase III of the FORMAT System is presented in this report. |
| 536 | ⊔ | ⊔ | ‡aAir Force Contract No. ‡bF33615-68-C-1633, Project No. 1467, Task No. 146705. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aStrains and stresses. |
| 650 | ⊔ | 0 | ‡aAirframes. |
| 650 | ⊔ | 0 | ‡aMatrices. |
| 650 | ⊔ | 0 | ‡aFORTRAN (Computer program language) |
| 650 | ⊔ | 0 | ‡aComputer programs. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡eissuing body. |
| 710 | 2 | ⊔ | ‡aAir Force Wright Aeronautical Laboratories, ‡esponsor. |
| 710 | 2 | ⊔ | ‡aDouglas Aircraft Company. ‡bAircraft Division, ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
| 899 | ⊔ | ⊔ | ‡a39015104956753 |
| CID | ⊔ | ⊔ | ‡a102893803 |
| DAT | 0 | ⊔ | ‡a20220802102022.0 ‡b20230928000000.0 |
| DAT | 1 | ⊔ | ‡a20230928062550.0 ‡b2024-08-06T17:32:14Z |
| CAT | ⊔ | ⊔ | ‡aSDR-MIU ‡cmiu ‡dALMA ‡lprepare.pl-004-008 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-miu.99187625981806381 ‡aMiU ‡bSDR ‡cGWLA ‡pmdp.39015104956753 ‡sMIU ‡199187625981806381 |
| 974 | ⊔ | ⊔ | ‡bMIU ‡cGWLA ‡d20240806 ‡sgoogle ‡umdp.39015104956753 ‡y1968 ‡rpd ‡qbib ‡tUS fed doc |