| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:752153039:1351 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:752153039:1351?format=raw |
LEADER: 01351nam a22003617a 4500
001 22885631
003 OR
008 940516r19851985dcu b f000 0 eng d
027 $aE-2685
035 $a10834334
040 $aGPO$cGPO$dDLC$dMvI
049 $aOREF$lbna
074 $a830-D (MF)
086 $aNAS 1.15:87093
086 0 $aNAS 1.15:87093
099 $aNAS 1.15:87093
100 1 $aHoyniak, Daniel.
245 10 $aForced response analysis of an aerodynamically detuned supersonic turbomachine rotor$h[microform] /$cDaniel Hoyniak and Sanford Fleeter.
260 $a[Washington, DC] :$bNational Aeronautics and Space Administration ;$a[Springfield, Va. :$bFor sale by the National Technical Information Service,$c1985]
300 $a1 v.
440 0 $aNASA technical memorandum ;$v87093.
533 $aMicrofiche.$b[Washington, D.C.? :$cNational Aeronautics and Space Administration],$d1985.$e1 microfiche.
500 $aDistributed to depository libraries in microfiche.
650 0 $aAeroelasticity.
650 0 $aUnsteady flow (Aerodynamics)
700 1 $aFleeter, Sanford.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.
907 $a.b17075166$bvdo $c-
902 $a040318
998 $b1$c981001$dm$ea$f-$g0
937 $aAssessment exclusion record.
999 $a19940516183014.0
945 $lvdonf$e1