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| 035 | ⊔ | ⊔ | ‡a(MiU)99187539621106381 |
| 035 | ⊔ | ⊔ | ‡asdr-miu.99187539621106381 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)423033568 |
| 035 | ⊔ | ⊔ | ‡a(GWLA)gwla ocn423033568 |
| 040 | ⊔ | ⊔ | ‡aLHL ‡beng ‡cLHL ‡dOCLCO ‡dOCLCQ ‡dOCLCF ‡dTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/46-2:79-3072 |
| 088 | ⊔ | ⊔ | ‡aADA 076493 |
| 088 | ⊔ | ⊔ | ‡aAFFDL TR 79-3072 |
| 100 | 1 | ⊔ | ‡aHinkle, T. V., ‡eauthor. |
| 245 | 1 | 0 | ‡aEffect of service environment on F-15 boron/epoxy stabilator / ‡cT.V. Hinkle. |
| 264 | ⊔ | 1 | ‡aWright-Patterson Air Force Base, Ohio : ‡bAir Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, ‡c1979. |
| 300 | ⊔ | ⊔ | ‡ax, 126 pages : ‡billustrations, tables ; ‡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 79-3072 |
| 500 | ⊔ | ⊔ | ‡aADA076493 (from http://www.dtic.mil). |
| 500 | ⊔ | ⊔ | ‡a"Final Technical Report August 1977 - June 1979." |
| 500 | ⊔ | ⊔ | ‡a"June 1979." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (page 126). |
| 520 | ⊔ | ⊔ | ‡aThe objective of this program was to conduct a series of tests for evaluating the effects of service environment on the strength of the boron/epoxy skins which are an integral part of the F-15 horizontal stabilator. Full scale static tests were conducted on two stabilators, and test results were compared with the capability of the F-15 stabilator demonstrated in previous testing. Moisture contents at various locations in the composite skins were predicted by evaluating the environmental histories of both test articles. Predicted contents were corroborated by moisture contents measured at conclusion of the static tests. F-15 deployments were projected for a 25-year service life, and moisture contents of stabilator composite skins were calculated for each projected deployment. Structural element tests were conducted under the maximum temperature and absorbed moisture conditions expected in service. Physical and chemical characteristics of the test article skins were evaluated relative to baseline boron/epoxy characteristics. |
| 536 | ⊔ | ⊔ | ‡aResearch supported by the Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, and performed by McDonnell Douglas Corporation, McDonnell Aircraft Company, under contract no. ‡bF33615-77-C-3124. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 7 | ‡aNondestructive testing. ‡2fast ‡0(OCoLC)fst01430903 |
| 650 | ⊔ | 7 | ‡aEpoxy compounds. ‡2fast ‡0(OCoLC)fst00914403 |
| 650 | ⊔ | 7 | ‡aComposite materials. ‡2fast ‡0(OCoLC)fst00871682 |
| 650 | ⊔ | 7 | ‡aBoron. ‡2fast ‡0(OCoLC)fst00836703 |
| 650 | ⊔ | 0 | ‡aNondestructive testing. |
| 650 | ⊔ | 0 | ‡aStatics ‡xTesting. |
| 650 | ⊔ | 0 | ‡aBoron. |
| 650 | ⊔ | 0 | ‡aEpoxy compounds. |
| 650 | ⊔ | 0 | ‡aComposite materials. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body. |
| 710 | 2 | ⊔ | ‡aMcDonnell Douglas Corporation, ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
| 899 | ⊔ | ⊔ | ‡a39015095319235 |
| CID | ⊔ | ⊔ | ‡a102855754 |
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| CAT | ⊔ | ⊔ | ‡aSDR-MIU ‡dALMA ‡lprepare.pl-004-008 |
| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bMIU ‡cGWLA ‡d20240214 ‡sgoogle ‡umdp.39015095319235 ‡y1979 ‡rpd ‡qbib ‡tUS fed doc |