| Record ID | marc_oregon_summit_records/catalog_files/osu_bibs.mrc:687546740:1507 |
| Source | Oregon Libraries |
| Download Link | /show-records/marc_oregon_summit_records/catalog_files/osu_bibs.mrc:687546740:1507?format=raw |
LEADER: 01507cam a2200397 i 4500
001 5687433
003 OR
008 940421s1979 dcua b f000 0 eng d
020 $cpbk.
035 $a10714314
037 $b22161
040 $aGPO$cGPO$dMvI-cor$dMvI
049 $aORE1$lbna
074 $a830-H-15
086 $aNAS 1.60:1406
086 0 $aNAS 1.60:1406
099 $aNAS 1.60:1406
100 1 $aCarlson, Harry W.
245 12 $aA modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack /$cHarry W. Carlson, Langley Research Center.
260 $aWashington :$bNational Aeronautics and Space Administration, Scientific and Technical Information Office ;$aSpringfield, Va. :$bfor sale by the National Technical Information Service,$c1979.
300 $a36 p. :$bill. ;$c27 cm.
490 1 $aNASA technical paper ; 1406.
500 $aFebruary 1979.
504 $aIncludes bibliographical references.
650 0 $aAerodynamic load.
650 0 $aSystem analysis.
650 0 $aAerodynamics, Supersonic.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Office.
710 2 $aLangley Research Center.
830 0 $aNASA technical paper ;$v1406.
907 $a.b16520300$bvdo $c-
902 $a990522
998 $b1$c981001$dm$ea$f-$g2
937 $aAssessment exclusion record.
999 $a19940421130627.0
945 $lvdog $e1