| Record ID | marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:63066993:1590 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:63066993:1590?format=raw |
LEADER: 01590nam a22003371a 4500
001 21968431
008 900706e1989 dcu b f000 0 eng d
027 $aL-16484
035 $a(GPO)90017448
040 $aGPO$cGPO$dMvI
049 $aNTEI
074 $a830-H-15 (MF)
086 0 $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 0 $a[Washington, D.C.] :$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 01 $aClosed form trim solution yielding minimum trim drag for airplanes with multiple longitudinal control effectors.
907 $a.b11926429$bwo $c-
902 $a071107
998 $b1$c980919$dm$ea$f-$g2
907 $a.b11926429
907 $a.b11926429
945 $lwoxau$aNAS 1.60:2907