| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:939970383:1841 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:939970383:1841?format=raw |
LEADER: 01841nam a22004697a 4500
001 32777874
003 OR
008 950817s1994 vau b f000 0 eng d
035 $a10920829
037 $aN 95-15898$bNASA
040 $aGPO$cGPO$dDLC
049 $aORE1$lbna
074 $a0830-D (MF)
086 $aNAS 1.15:109152
086 0 $aNAS 1.15:109152
099 $aNAS 1.15:109152
100 1 $aHolland, Scott Douglas,$d1964-
245 10 $aWind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6$h[microform] /$cScott D. Holland.
246 3 $aWind tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6.
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 $aNASA technical memorandum ;$v109152.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1994]$e1 microfiche.
500 $aDistributed to depository libraries in microfiche.
500 $aShipping list no.: 95-0276-M.
650 7 $aActuators.$2nasat.
650 7 $aBlocking.$2nasat.
650 7 $aCowlings.$2nasat.
650 7 $aEngine inlets.$2nasat.
650 7 $aHypersonic inlets.$2nasat.
650 7 $aHypersonic wind tunnels.$2nasat.
650 7 $aInlet flow.$2nasat.
650 7 $aShock wave interaction.$2nasat.
650 7 $aSupersonic combustion ramjet engines.$2nasat.
650 7 $aWind tunnel tests.$2nasat.
710 2 $aLangley Research Center.
907 $a.b18469371$bvdo $c-
902 $a020220
998 $b1$c981001$dm$ea$f-$g0
937 $aAssessment exclusion record.
999 $a19950817111545.0
945 $lvdonf$e1