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| 001 | 102856561 | ||
| 003 | MiAaHDL | ||
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| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 090622e196604 ohua bt f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡a(MiU)99187539640706381 |
| 035 | ⊔ | ⊔ | ‡asdr-miu.99187539640706381 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)405684983 |
| 035 | ⊔ | ⊔ | ‡a(GWLA)gwla ocn405684983 |
| 040 | ⊔ | ⊔ | ‡aLHL ‡beng ‡cLHL ‡dOCLCO ‡dOCLCQ ‡dOCLCF ‡dTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/46-2:66-16 |
| 088 | ⊔ | ⊔ | ‡aAD 0485307 |
| 088 | ⊔ | ⊔ | ‡aAFFDL TR 66-16 |
| 110 | 2 | ⊔ | ‡aMartin Company, ‡eauthor. |
| 245 | 1 | 0 | ‡aMathematical analysis of heat conduction in a sector of a hollow circular cylinder / ‡cMartin Company, Orlando Division, Enginering Mechanics Research Laboratory. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, ‡c1966. |
| 300 | ⊔ | ⊔ | ‡ax, 138 pages : ‡billustrations ; ‡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 66-16 |
| 500 | ⊔ | ⊔ | ‡aAD0485307 (from http://www.dtic.mil). |
| 500 | ⊔ | ⊔ | ‡a"April 1966." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (pages 137-138). |
| 520 | ⊔ | ⊔ | ‡aThe temperature distribution within a sector of a hollow circular cylinder with temperature dependent thermophysical properties was analyzed based on exact mathematical solution. The subject nonlinear differential equation was reduced to a linear differential equation by an integral transform and with the assumption that only the thermal conductivity is a function of temperature whereas the thermal diffusivity remains constant. The solution was programmed in FORTRAN 4 for application to an IBM 7094. In addition, a successive transform applicable to the solution of similar problems involving temperature dependent thermal diffusivity is illustrated and discussed. |
| 536 | ⊔ | ⊔ | ‡aResearch supported by the Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, and performed by the Martin Company, Orlando Division, Engineering Mechanics Research Laboratory under contract ‡bAF33(615)-2385. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 7 | ‡aMathematical analysis. ‡2fast ‡0(OCoLC)fst01012068 |
| 650 | ⊔ | 7 | ‡aDifferential equations, Nonlinear. ‡2fast ‡0(OCoLC)fst00893474 |
| 650 | ⊔ | 0 | ‡aDifferential equations, Nonlinear. |
| 650 | ⊔ | 0 | ‡aMathematical analysis. |
| 650 | ⊔ | 0 | ‡aCylinders ‡xThermal conductivity. |
| 650 | ⊔ | 0 | ‡aPipe ‡xThermal conductivity. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor. |
| 899 | ⊔ | ⊔ | ‡a39015095310358 |
| CID | ⊔ | ⊔ | ‡a102856561 |
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| DAT | 1 | ⊔ | ‡a20220411060511.0 ‡b2024-04-29T17:30:36Z |
| DAT | 2 | ⊔ | ‡a2024-04-29T17:30:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-MIU ‡dALMA ‡lprepare.pl-004-008 |
| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bMIU ‡cGWLA ‡d20240429 ‡sgoogle ‡umdp.39015095310358 ‡y1966 ‡rpd ‡qbib ‡tUS fed doc |