| Record ID | marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:64540707:1545 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/washs02192008.mrc_revrev.mrc:64540707:1545?format=raw |
LEADER: 01545nam a22003491a 4500
001 22237590
008 900817r19861984dcu b f000 0 eng d
027 $aL-15787
035 $a(GPO)90019409
040 $aGPO$cGPO$dMvI
049 $aNTEI
074 $a830-H-15 (MF)
086 0 $aNAS 1.60:2336
100 1 $aPittman, Jimmy L.
245 10 $aSupersonic, nonlinear, attached-flow wing design for high lift with experimental validation$h[microfiche] /$cJames L. Pittman and David S. Miller, William H. Mason.
260 0 $a[Washington, D.C.] :$bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ;$a[Springfield, Va. :$bFor sale by the National Technical Information Service],$c1984.
300 $a1 v.
440 0 $aNASA technical paper ;$v2336.
533 $aMicrofiche.$b[Washington, D.C.? :$cNational Aeronautics and Space Administration],$d1986.$e3 microfiches.
500 $aDistributed to depository libraries in microfiche.
650 0 $aAirplanes$xWings.
650 0 $aAerodynamics, Supersonic.
700 1 $aMiller, David S.
700 1 $aMason, William H.$q(William Henry),$d1947-
710 1 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch.
740 01 $aSupersonic, nonlinear, attached flow wing design for high lift with experimental validation.
907 $a.b11946891$bwo $c-
902 $a071029
998 $b1$c980919$dm$ea$f-$g0
907 $a.b11946891
907 $a.b11946891
945 $lwoxau$aNAS 1.60:2336