| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:702728362:1522 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:702728362:1522?format=raw |
LEADER: 01522cam a2200397 a 4500
001 7325143
003 OR
008 940423s1980 dcua b f000 0 eng d
035 $a10729241
040 $aGPO$cGPO$dMvI
049 $aOREF$lbna
074 $a830-H-15 (MF)
086 $aNAS 1.60:1767
086 0 $aNAS 1.60:1767
099 $aNAS 1.60:1767
100 1 $aPittman, Jimmy L.
245 10 $aExperimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /$cJimmy L. Pittman and Gregory D. Riebe.
260 $a[Washington, D.C.] :$bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ;$a[Springfield, Va. :$bFor sale by the National Technical Information Service],$c1980.
300 $a113 p. :$bill. ;$c27 cm.
440 0 $aNASA technical paper ;$v1767.
500 $a"Langley Research Center."
500 $aDec. 1980.
504 $aIncludes bibliographical references.
650 0 $aAerodynamics, Supersonic.
650 0 $aHypersonic planes.
650 0 $aSupersonic wind tunnels.
650 0 $aMach number.
700 1 $aRiebe, Gregory D.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch.
710 2 $aLangley Research Center.
907 $a.b16660225$bvmi $c-
902 $a040817
998 $b1$c981001$dm$ea$f-$g0
937 $aAssessment exclusion record.
999 $a19940423150903.0
945 $lvminf$e1