| LDR | 02624cam a2200529 a 4500 | ||
| 001 | 100393404 | ||
| 003 | MiAaHDL | ||
| 005 | 20240920000000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 110328s1955 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡a(MiU)990131340930106381 |
| 035 | ⊔ | ⊔ | ‡asdr-miu.990131340930106381 |
| 035 | ⊔ | ⊔ | ‡z(MiU)MIU01000000000000013134093-goog |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)709606536 |
| 035 | ⊔ | ⊔ | ‡z(MiU)Aleph013134093 |
| 040 | ⊔ | ⊔ | ‡aCSL ‡beng ‡cTEF ‡dNACAR ‡dOCLCF ‡dOCLCQ ‡dOCLCO ‡dOCLCQ ‡dOCLCL |
| 049 | ⊔ | ⊔ | ‡aEYMG |
| 050 | ⊔ | 4 | ‡aTL678 ‡b.G89 1955 |
| 086 | 0 | ⊔ | ‡aY 3.N21/5:15/L54K16a |
| 100 | 1 | ⊔ | ‡aGuy, Lawrence D. ‡q(Lawrence Duncan), ‡d1921- |
| 245 | 1 | 0 | ‡aEffects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60° delta wing at Mach numbers from 0.75 to 1.96 / ‡cby Lawrence D. Guy and Hoyt V. Brown. |
| 260 | ⊔ | ⊔ | ‡aWashington [D.C.] : ‡bNational Advisory Committee for Aeronautics, ‡c[1955] |
| 300 | ⊔ | ⊔ | ‡a35 pages : ‡billustrations ; ‡c27 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aNACA research memorandum ; ‡vL54K16a |
| 500 | ⊔ | ⊔ | ‡a"Classification changed to unclassified, authority: NASA publication annoucement no. 3, effective date: December 3, 1958"--Stamped on cover. |
| 500 | ⊔ | ⊔ | ‡a"Confidential." |
| 500 | ⊔ | ⊔ | ‡a"February, 15, 1955." |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical reference (pages 13-14). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 7 | ‡aTrailing edges (Aerodynamics) ‡2fast ‡0(OCoLC)fst01154417 |
| 650 | ⊔ | 7 | ‡aTrailing edge flaps. ‡2fast ‡0(OCoLC)fst01154416 |
| 650 | ⊔ | 7 | ‡aHinge moments (Aerodynamics) ‡2fast ‡0(OCoLC)fst00957213 |
| 650 | ⊔ | 7 | ‡aAirplanes ‡xWings, Triangular. ‡2fast ‡0(OCoLC)fst00803564 |
| 650 | ⊔ | 7 | ‡aAirplanes ‡xControl systems ‡xTesting. ‡2fast ‡0(OCoLC)fst00803123 |
| 650 | ⊔ | 0 | ‡aTrailing edges (Aerodynamics) |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xWings, Triangular. |
| 650 | ⊔ | 0 | ‡aTrailing edge flaps. |
| 650 | ⊔ | 0 | ‡aHinge moments (Aerodynamics) |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xControl systems ‡xTesting. |
| 700 | 1 | ⊔ | ‡aBrown, Hoyt V. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Advisory Committee for Aeronautics. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
| 758 | ⊔ | ⊔ | ‡ihas work: ‡aEffects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60° delta wing at Mach numbers from 0.75 to 1.96 (Text) ‡1https://id.oclc.org/worldcat/entity/E39PCFXqcdwF8HFKrdt8Xx7M8C ‡4https://id.oclc.org/worldcat/ontology/hasWork |
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| CID | ⊔ | ⊔ | ‡a100393404 |
| DAT | 0 | ⊔ | ‡a20240919091841.0 ‡b20240920000000.0 |
| DAT | 1 | ⊔ | ‡a20240920060553.0 ‡b2024-09-20T13:15:10Z |
| DAT | 2 | ⊔ | ‡a2024-03-16T17:30:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-MIU ‡cmiu ‡dALMA ‡lprepare.pl-004-008 |
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| 974 | ⊔ | ⊔ | ‡bMIU ‡cGWLA ‡d20240920 ‡sgoogle ‡umdp.39015086506998 ‡y1955 ‡rpd ‡qbib ‡tUS fed doc |