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| 035 | ⊔ | ⊔ | ‡a(OCoLC)55602127 |
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| 049 | ⊔ | ⊔ | ‡aUIUU |
| 100 | 1 | ⊔ | ‡aFortini, Anthony. |
| 245 | 1 | 0 | ‡aComparison of experimental to predicted heat transfer in a bell-shaped nozzle with upstream flow disturbances / ‡cAnthony Fortini and Robert C. Ehlers. |
| 246 | 3 | ⊔ | ‡aNASA TN D-1743 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, ‡c1963. |
| 300 | ⊔ | ⊔ | ‡a36 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical note ; ‡vD-1743 |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 12-13). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aFilm coefficients (Physics) |
| 650 | ⊔ | 0 | ‡aHeat ‡xTransmission. |
| 650 | ⊔ | 0 | ‡aRocket engines. |
| 650 | ⊔ | 0 | ‡aRockets (Aeronautics) |
| 700 | 1 | ⊔ | ‡aEhlers, Robert C. |
| 710 | 2 | ⊔ | ‡aLewis Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
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| DAT | 2 | ⊔ | ‡a2024-01-24T18:30:02Z ‡b2023-09-29T20:00:02Z |
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