| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:1197144621:1650 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:1197144621:1650?format=raw |
LEADER: 01650nam a22004337a 4500
001 42623873
003 OCoLC
005 19991012154814.0
008 991012s1999 vau b f000 0 eng d
035 $a(GPO)99027463
037 $a19990047898$bNASA
040 $aGPO$cGPO$dDLC$dMvI
049 $aORE1
074 $a0830-H-14 (MF)
086 0 $aNAS 1.26:209328
086 0 $aNAS 1.26:209328
100 1 $aHassan, Ahmed.
245 10 $aPredicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap$h[microform] /$cAhmed Hassan.
260 $aHampton, Va. :$bNational Aeronautics and Space Administration, Langley Research Center ;$a[Springfield, Va. :$bNational Technical Information Service, distributor,$c1999]
300 $a1 v.
490 1 $a[NASA contractor report] ;$vNASA/CR-1999-209328.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1999]$e2 microfiches.
500 $aShipping list no.: 99-0933-M.
650 7 $aNoise reduction.$2nasat.
650 7 $aAirfoils.$2nasat.
650 7 $aBlade-vortex interaction.$2nasat.
650 7 $aNavier-Stokes equation.$2nasat.
650 7 $aTrailing edge flaps.$2nasat.
650 7 $aAerodynamic characteristics.$2nasat.
650 7 $aGrid generation (Mathematics)$2nasat.
650 7 $aComputational grids.$2nasat.
710 2 $aLangley Research Center.
830 0 $aNASA contractor report ;$vNASA CR-209328.
907 $a.b20535545$bvdo $cv
902 $a010129
998 $b2$c991120$dm$ea$fv$g0
935 $atmp97159756
937 $aAssessment exclusion record.
945 $lvdonf$e1