| LDR | 01316cam a2200337Ia 4500 | ||
| 001 | 011424888 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 930827s1974 dcua b f000 0 eng d | ||
| 029 | 1 | ⊔ | ‡aGBVCP ‡b607586885 |
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6360226 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)28706071 |
| 040 | ⊔ | ⊔ | ‡aABC ‡cABC ‡dLHL |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL521.3.T4 ‡bA3 no. 3030 |
| 086 | 0 | ⊔ | ‡aNAS 1.15:X-3030 |
| 100 | 1 | ⊔ | ‡aMcClinton, Charles R. |
| 245 | 1 | 0 | ‡aEffect of ratio of wall boundary-layer thickness to jet diameter on mixing of a normal hydrogen jet in a supersonic stream / ‡cby Charles R. McClinton. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1974. |
| 300 | ⊔ | ⊔ | ‡a42 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical memorandum ; ‡vNASA TM X-3030 |
| 500 | ⊔ | ⊔ | ‡aPrepared at Langley Research Center. |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 13-14). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAerodynamics, Supersonic. |
| 650 | ⊔ | 0 | ‡aBoundary layer. |
| 650 | ⊔ | 0 | ‡aJets ‡xFluid dynamics. |
| 650 | ⊔ | 0 | ‡aFuel pumps. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xRamjet engines. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| CID | ⊔ | ⊔ | ‡a011424888 |
| DAT | 0 | ⊔ | ‡a20101004143744.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112164151.0 ‡b2023-03-14T18:19:51Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6360226 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106612697 ‡sUIU ‡16360226 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106612697 ‡y1974 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |