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| 008 | 121113s1953 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡a(MiU)990128619640106381 |
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| 035 | ⊔ | ⊔ | ‡z(MiU)MIU01000000000000012861964-goog |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)817733246 |
| 035 | ⊔ | ⊔ | ‡z(MiU)Aleph012861964 |
| 040 | ⊔ | ⊔ | ‡aNACAR ‡cNACAR ‡dUtOrBLW |
| 049 | ⊔ | ⊔ | ‡aNACA |
| 086 | 0 | ⊔ | ‡aY 3.N21/5:15/L53I29b |
| 100 | 1 | ⊔ | ‡aBromm, August F. |
| 245 | 1 | 0 | ‡aInvestigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag / ‡cby August F. Bromm, Jr., and Julia M. Goodwin. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1953. |
| 300 | ⊔ | ⊔ | ‡a20 p. : ‡bill. ; ‡c27 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aNational Advisory Committee for Aeronautics research memorandum ; ‡vL53I29b |
| 500 | ⊔ | ⊔ | ‡a"December 1, 1953." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 10). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aBody of revolution. ‡0http://id.loc.gov/authorities/subjects/sh85015251 |
| 650 | ⊔ | 0 | ‡aAerodynamics, Supersonic. ‡0http://id.loc.gov/authorities/subjects/sh85001297 |
| 650 | ⊔ | 0 | ‡aSkin friction (Aerodynamics) ‡0http://id.loc.gov/authorities/subjects/sh85123197 |
| 650 | ⊔ | 0 | ‡aBase flow (Aerodynamics) ‡0http://id.loc.gov/authorities/subjects/sh85012023 |
| 650 | ⊔ | 0 | ‡aDrag (Aerodynamics) ‡0http://id.loc.gov/authorities/subjects/sh85039270 |
| 700 | 1 | ⊔ | ‡aGoodwin, Julia M. |
| 710 | 2 | ⊔ | ‡aLangley Aeronautical Laboratory. ‡0http://id.loc.gov/authorities/names/n81018841 ‡1http://id.loc.gov/rwo/agents/n81018841 |
| 710 | 2 | ⊔ | ‡aUnited States. ‡bNational Adviosry Committee for Aeronautics. ‡tNACA research memorandum. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
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