| Record ID | marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:111632838:1582 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:111632838:1582?format=raw |
LEADER: 01582nam a2200373Ka 4500
001 28249819
003 aOCoLC
005 19950727063724.6
008 930610s1992 dcu b f000 0 eng d
035 $aWSU000844250
035 $aocm28249819
037 $aN 93-13353$bNASA
040 $aGPO$cGPO$dNTE$dWaOLN
074 $a0830-H-15 (MF)
086 0 $aNAS 1.60:3253
100 1 $aErickson, Gary E.
245 10 $aEffects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 55⁰ cropped delta wing$h[microform] /$cGary E. Erickson, Lawrence W. Rogers.
260 $a[Washington, DC] :$bNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;$a[Springfield, Va. :$bFor sale by the National Technical Information Service],$c1992.
300 $a1 v.
490 1 $aNASA technical paper ;$v3253.
500 $aDistributed to depository libraries in microfiche.
500 $aShipping list no.: 93-0355-M.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration],$d1992.$e2 microfiches.
650 0 $aAerodynamics, Supersonic.
650 0 $aAirplanes$xWings, Triangular.
700 1 $aRogers, Lawrence W.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program.
830 0 $aNASA technical paper ;$v3253.
907 $a.b12756337$bwo $c-
902 $a050826
998 $b2$c950717$dm$ea$f-$g0
940 $lWO
940 $lEJ
945 $lwoxau$aNAS 1.60:3253