Record ID | marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:1451570301:1375 |
Source | Oregon Libraries |
Download Link | /show-records/marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:1451570301:1375?format=raw |
LEADER: 01375nam a2200325Ka 4500
001 43263577
003 OCoLC
005 20000222171211.0
007 he bmb024bbca
008 000112s1999 vau b f000 0 eng d
037 $a19990100650$bNASA
040 $aGPO$cGPO$dNTE
049 $aNTEI
074 $a0830-D (MF)
086 0 $aNAS 1.15:209513
100 1 $aAsbury, Scott C.
245 10 $aStatic performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control$h[microform] /$cScott C. Asbury and Craig A. Hunter.
246 2 $aStatic performance of a fixed geometry exhaust nozzle incorporating porous cavities for shock boundary layer interaction control.
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 $aNASA/TM ;$v1999-209513.
500 $aShipping list no.: 2000-0197-M.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1999]$e2 microfiches.
700 1 $aHunter, Craig A.
710 2 $aLangley Research Center.
830 0 $aNASA technical memorandum ;$v209513.
907 $a.b27682870$bwo $c-
902 $a000223
998 $b1$c000223$dm$ea$f-$g0
945 $lwoxau$aNAS 1.15:209513