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| 003 | MiAaHDL | ||
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| 008 | 220706s1991 tnua bt f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡a(MiU)99187625235006381 |
| 035 | ⊔ | ⊔ | ‡asdr-miu.99187625235006381 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)1334605411 |
| 035 | ⊔ | ⊔ | ‡a(GWLA)gwla on1334605411 |
| 040 | ⊔ | ⊔ | ‡aTRAAL ‡beng ‡erda ‡cTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/33: 91-008 |
| 100 | 1 | ⊔ | ‡aSuhs, N. E., ‡eauthor. |
| 245 | 1 | 0 | ‡aPEGSUS 4.0 User's Manual / ‡cN.E. Suhs and R.W. Tramel. |
| 264 | ⊔ | 1 | ‡aArnold Air Force Base, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1991. |
| 300 | ⊔ | ⊔ | ‡a234 pages : ‡billustrations, ‡c28 cm |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aAEDC-TR ; ‡v91-008 |
| 500 | ⊔ | ⊔ | ‡aReport was prepared by Calspan Corporation. |
| 500 | ⊔ | ⊔ | ‡a"Final Report: March 1, 1990 through June 30, 1991." |
| 500 | ⊔ | ⊔ | ‡a"November 1991." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliograqphic references (pages 36-37). |
| 520 | ⊔ | ⊔ | ‡aMany aerodynamic configurations are too complex to be represented by a single computational mesh. A multiple-mesh domain decomposition method called chimera has been developed to allow complex aerodynamic configurations to be modeled by a system of individually generated meshes, each representing a component of the overall configuration. The chimera approach requires the use of two computer codes, PEGSUS and a flow solver. PEGSUS calculates the interactions among the meshes and produces a file consisting of interpolation information that is used by the flow solver to obtain a global flow-field solution for the entire mesh system. This report documents the design and use of the latest version (4.0) of PEGSUS, and describes techniques for proper modeling of complex aerodynamic configurations. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aComputational grids (Computer systems) |
| 650 | ⊔ | 0 | ‡aComputational fluid dynamics. |
| 700 | 1 | ⊔ | ‡aTramel, R. W., ‡eauthor. |
| 710 | 2 | ⊔ | ‡aCalspan Corporation, ‡esponsor. |
| 710 | 2 | ⊔ | ‡aArnold Engineering Development Center, ‡esponsor. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
| 899 | ⊔ | ⊔ | ‡a39015104951903 |
| CID | ⊔ | ⊔ | ‡a102893554 |
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| DAT | 2 | ⊔ | ‡a2024-07-29T17:30:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-MIU ‡cmiu ‡dALMA ‡lprepare.pl-004-008 |
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| 974 | ⊔ | ⊔ | ‡bMIU ‡cGWLA ‡d20241208 ‡sgoogle ‡umdp.39015104951903 ‡y1991 ‡rpd ‡qbib ‡tUS fed doc |