| Record ID | ia:aerodynamicperfo00moor |
| Source | Internet Archive |
| Download MARC XML | https://archive.org/download/aerodynamicperfo00moor/aerodynamicperfo00moor_marc.xml |
| Download MARC binary | https://www.archive.org/download/aerodynamicperfo00moor/aerodynamicperfo00moor_meta.mrc |
LEADER: 01173cam 2200277Ia 4500
001 6368645
005 20101011145310.0
008 821213s1979 dcua b f000 0 eng d
035 $a(OCoLC)ocm09048453
040 $aGPO$cGPO$dABC$dOCLCQ
050 4 $aTL521.3$b.N18 no. 1510
074 $a830-H-15 (microfiche)
086 0 $aNAS 1.60:1510
049 $aUIUU
100 1 $aMoore, Royce D.
245 10 $aAerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /$cRoyce D. Moore and Lonnie Reid.
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],$c1979.
300 $a40 p. :$bill. ;$c27 cm.
440 0 $aNASA technical paper ;$v1510
500 $a"September 1979"--Cover.
504 $aIncludes bibliographical references (p. 12).
650 0 $aFans (Machinery)$xPerformance.
650 0 $aTurbomachines$xAerodynamics.
700 1 $aReid, Lonnie.
710 1 $aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch.
994 $aC0$bUIU