| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:743876548:1676 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:743876548:1676?format=raw |
LEADER: 01676nam a22003731a 4500
001 21968431
003 OR
008 940514e1989 dcu b f000 0 eng d
027 $aL-16484
035 $a10827792
040 $aGPO$cGPO$dMvI
049 $aOREF$lbna
074 $a830-H-15 (MF)
086 $aNAS 1.60:2907
086 0 $aNAS 1.60:2907
099 $aNAS 1.60:2907
100 1 $aGoodrich, Kenneth H.
245 12 $aA closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors$h[microform] /$cKenneth H. Goodrich, Steven M. Sliwa, and Frederick J. Lallman.
260 $a[Washington, D.C.] :$bNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;$a[Springfield, Va. :$bFor sale by the National Technical Information Service],$c1989.
300 $a1 v.
440 0 $aNASA technical paper ;$v2907.
533 $aMicrofiche.$b[Washington, D.C.? :$cNational Aeronautics and Space Administration],$d1989.$e1 microfiche ; 11 x 15 cm.
500 $aDistributed to depository libraries in microfiche.
650 0 $aAirplanes$xDesign and construction.
700 1 $aSliwa, Steven M.
700 1 $aLallman, Frederick J.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Division.
740 0 $aClosed form trim solution yielding minimum trim drag for airplanes with multiple longitudinal control effectors.
907 $a.b17012107$bvmi $c-
902 $a040817
998 $b1$c981001$dm$ea$f-$g2
937 $aAssessment exclusion record.
999 $a19940514230116.0
945 $lvminf$e1