| Record ID | marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:996813911:1599 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:996813911:1599?format=raw |
LEADER: 01599nam a2200445Ka 4500
001 32028496
003
005 19950929135402.5
007 heubmb024bbca
008 950221s1994 vau b f000 0 eng d
035 $aWSU000897328
037 $aN 94-34172$bNASA
040 $aGPO$cGPO$dNTE$dWaOLN
049 $aNTEK$lMicrofiche
074 $a0830-H-15 (MF)
086 0 $aNAS 1.60:3411
100 1 $aWing, David J.
245 10 $aStatic performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept$h[microform] /$cDavid J. Wing.
260 $aHampton, Va. :$bNational Aeronautics and Space Administration, Langley Research Center ;$a[Springfield, Va. :$bNational Technical Information Service, distributor,$c1994]
300 $a1 v.
440 0 $aNASA technical paper ;$v3411.
500 $aDistributed to depository libraries in microfiche.
500 $aShipping list no.: 94-0821-M.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1994]$e2 microfiches.
650 0 $aJet nozzles$xTesting.
650 7 $aExhaust nozzles.$2nasat.
650 7 $aNozzle geometry.$2nasat.
650 7 $aSkewness.$2nasat.
650 7 $aSonic nozzles.$2nasat.
650 7 $aStatic tests.$2nasat.
650 7 $aThroats.$2nasat.
650 7 $aThrust vector control.$2nasat.
650 7 $aWind tunnel tests.$2nasat.
710 2 $aLangley Research Center.
907 $a.b21578710$bwo $c-
902 $a040715
998 $b1$c950717$dm$ea$f-$g0
907 $a.b21578710
940 $lWO
945 $lwoxau$aNAS 1.60:3411