| LDR | 01276cam a2200325Ia 4500 | ||
| 001 | 011423833 | ||
| 003 | MiAaHDL | ||
| 005 | 20141013010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 910814s1991 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6354179 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)24233960 |
| 040 | ⊔ | ⊔ | ‡aABC ‡cABC ‡dLHL |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.60:3099 |
| 090 | ⊔ | ⊔ | ‡aTL521.3 ‡b.N18 no. 3099 |
| 100 | 1 | ⊔ | ‡aPlentovich, Elizabeth B. |
| 245 | 1 | 0 | ‡aEffects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds / ‡cE.B. Plentovich, Julio Chu, and M.B. Tracy. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1991. |
| 300 | ⊔ | ⊔ | ‡a51 p. ; ‡c28 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical paper ; ‡v3099 |
| 500 | ⊔ | ⊔ | ‡aPrepared at Langley Research Center. |
| 504 | ⊔ | ⊔ | ‡aBibliography: p. 5-6. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aTurbulent boundary layer. |
| 650 | ⊔ | 0 | ‡aAerodynamics, Transonic. |
| 650 | ⊔ | 0 | ‡aAerodynamic load. |
| 650 | ⊔ | 0 | ‡aCavities (Airplanes) |
| 650 | ⊔ | 0 | ‡aReynolds number. |
| 650 | ⊔ | 0 | ‡aYawing (Aerodynamics) |
| 700 | 1 | ⊔ | ‡aTracy, M. B. |
| 700 | 1 | ⊔ | ‡aChu, Julio. |
| CID | ⊔ | ⊔ | ‡a011423833 |
| DAT | 0 | ⊔ | ‡a20100930143021.0 ‡b20141013010000.0 |
| DAT | 1 | ⊔ | ‡a20141112173021.0 ‡b2023-03-14T18:26:52Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6354179 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106710962 ‡sUIU ‡16354179 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106710962 ‡y1991 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |