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| 040 | ⊔ | ⊔ | ‡aNACAR ‡beng ‡cNACAR ‡dOCLCO ‡dOCLCF ‡dOCLCO ‡dOCLCQ ‡dOCLCO ‡dOCLCQ ‡dOCLCO ‡dUtOrBLW |
| 049 | ⊔ | ⊔ | ‡aEYMG |
| 086 | 0 | ⊔ | ‡aY 3.N21/5:15/L53H31 |
| 100 | 1 | ⊔ | ‡aJaquet, Byron M. |
| 245 | 1 | 0 | ‡aSome low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35° swept-wing model and an unswept-wing model / ‡cby Byron M. Jaquet. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1953. |
| 300 | ⊔ | ⊔ | ‡a43 pages : ‡billustrations ; ‡c27 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aNational Advisory Committee for Aeronautics research memorandum ; ‡vL53H31 |
| 500 | ⊔ | ⊔ | ‡a"October 20, 1953." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (page 12). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 7 | ‡aStability of airplanes, Longitudinal. ‡2fast ‡0http://id.worldcat.org/fast/1131217 |
| 650 | ⊔ | 7 | ‡aAirplanes ‡xWings, Swept-back. ‡2fast ‡0http://id.worldcat.org/fast/803560 |
| 650 | ⊔ | 7 | ‡aAirplanes ‡xWings. ‡2fast ‡0http://id.worldcat.org/fast/803545 |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xWings. ‡0http://id.loc.gov/authorities/subjects/sh85002923 |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xWings, Swept-back. ‡0http://id.loc.gov/authorities/subjects/sh85002928 |
| 650 | ⊔ | 0 | ‡aStability of airplanes, Longitudinal. ‡0http://id.loc.gov/authorities/subjects/sh85127188 |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Adviosry Committee for Aeronautics. ‡tNACA research memorandum. |
| 710 | 2 | ⊔ | ‡aLangley Aeronautical Laboratory. ‡0http://id.loc.gov/authorities/names/n81018841 ‡1http://id.loc.gov/rwo/agents/n81018841 |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
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