| Record ID | marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:1632258815:1805 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:1632258815:1805?format=raw |
LEADER: 01805cam a2200385Ka 4500
001 51617379
003 OCoLC
005 20030403091512.0
008 030210s2001 vau b f000 0 eng d
037 $a20010047400$bNASA
040 $aGPO$cGPO$dNTE
049 $aNTEI$aNTEF
074 $a0830-H-15 (MF)
074 $a0830-H-15 (online)
086 0 $aNAS 1.60:210629
245 00 $aFlight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds /$cJohn E. Lamar ... [et al.].
246 2 $aFlight, wind tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds.
260 $aHampton, Va. :$bNational Aeronautics and Space Administration, Langley Research Center ;$aHanover MD :$bAvailable from NASA Center for AeroSpace Information (CASI),$c[2001]
300 $a1 v.
490 1 $aNASA/TP ;$v2001-210629.
538 $aSystem requirements: Adobe Acrobat Reader.
500 $aShipping list no.: 2003-0098-M.
530 $aAlso available via Internet from the NASA web site. Address as of 2/10/03: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tp/NASA-2001-tp210629.pdf ; current access is available via PURL.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d2002?]$e2 microfiches.
650 0 $aAerodynamics.
700 1 $aLamar, John E.
710 2 $aLangley Research Center.
830 0 $aNASA technical paper ;$v210629.
856 41 $zOnline access for everyone$uhttp://purl.access.gpo.gov/GPO/LPS26671
907 $a.b30188271$bmulti$c-
902 $a080125
998 $b2$c030403$dm$ea$f-$g0
907 $a.b30188271
945 $lwoxau$aNAS 1.60:210629
945 $lt $aNAS 1.60:210629 (Electronic resource)