| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:713036138:1328 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:713036138:1328?format=raw |
LEADER: 01328cam a2200361 a 4500
001 8355021
003 OR
008 940425s1981 dcua b f000 0 eng d
035 $a10739505
040 $aGPO$cGPO$dMvI
043 $an-us---
049 $aOREF$lbna
074 $a830-H-15 (MF)
086 $aNAS 1.60:1866
086 0 $aNAS 1.60:1866
099 $aNAS 1.60:1866
100 1 $aJohnson, Gary M.
245 10 $aSurrogate-equation technique for simulation of steady inviscid flow /$cGary M. Johnson.
260 $aWashington, D.C. :$bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ;$a[Springfield, Va. :$bFor sale by the National Technical Information Service],$c1981.
300 $a37 p. :$bill. ;$c27 cm.
440 0 $aNASA technical paper ;$v1886.
500 $a"Lewis Research Center."
500 $a"September 1981"--Cover.
504 $aIncludes bibliographical references.
650 0 $aAerodynamics$xMathematical models.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch.
710 2 $aLewis Research Center.
907 $a.b16753501$bvmi $c-
902 $a040817
998 $b1$c981001$dm$ea$f-$g0
937 $aAssessment exclusion record.
999 $a19940425080821.0
945 $lvminf$e1