| LDR | 01355nam a2200325Ia 4500 | ||
| 001 | 011430558 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 961018s1974 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6384377 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)35762128 |
| 040 | ⊔ | ⊔ | ‡aABC ‡cABC |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL521.3.C6 ‡bA3 no. 2436 |
| 086 | 0 | ⊔ | ‡aNAS 1.26:2436 |
| 100 | 1 | ⊔ | ‡aPfenninger, W. |
| 245 | 1 | 0 | ‡aReduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction / ‡cby W. Pfenninger and J. Syberg. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1974. |
| 300 | ⊔ | ⊔ | ‡aiii, 303 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA contractor report ; ‡vNASA CR-2436 |
| 500 | ⊔ | ⊔ | ‡a"Prepared by Boeing Commercial Airplane Company ... for Langley Research Center." |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 86-92). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aLaminar flow. |
| 650 | ⊔ | 0 | ‡aBoundary layer. |
| 650 | ⊔ | 0 | ‡aJet nozzles ‡xNoise. |
| 650 | ⊔ | 0 | ‡aSupersonic wind tunnels. |
| 700 | 1 | ⊔ | ‡aSyberg, J. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| 710 | 2 | ⊔ | ‡aBoeing Commercial Airplane Company. |
| CID | ⊔ | ⊔ | ‡a011430558 |
| DAT | 0 | ⊔ | ‡a20101026084804.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112164151.0 ‡b2023-03-14T18:17:54Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6384377 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106582825 ‡sUIU ‡16384377 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106582825 ‡y1974 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |