| Record ID | bcl_marc/bcl_open.03.mrc:211660944:1493 |
| Source | bcl_marc |
| Download Link | /show-records/bcl_marc/bcl_open.03.mrc:211660944:1493?format=raw |
LEADER: 01493nam 22003617a 4500
004 GPQ1265
005 20000524102400.0
008 990810s1999 vau b f000 0 eng d
035 $a(OCoLC)ocm42046411
035 9 $aGPQ1265
037 $a19990031948$bNASA
040 $aGPO$cGPO$dDLC$dMvI
049 $aBXMX
074 $a0830-D (MF)
086 0 $aNAS 1.15:209104
100 1 $aBennett, Robert M.$q(Robert Merrill),$d1945-
245 10 $aComputational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations$h[microform] /$cRobert M. Bennett and Charlotte E. Walker.
260 $aHampton, Va. :$bNational Aeronautics and Space Administration, Langley Research Center ;$aSpringfield, VA :$bNational Technical Information Service, distributor,$c[1999]
300 $a1 v.
490 1 $a[NASA technical memorandum] ;$vNASA/TM-1999-209104
500 $aShipping list no.: 99-0729-M.
533 $aMicrofiche.$b[Washington, D.C. :$cNational Aeronautics and Space Administration,$d1999]$e1 microfiche.
650 7 $aComputational fluid dynamics.$2nasat
650 7 $aDelta wings.$2nasat
650 7 $aAirfoil profiles.$2nasat
650 7 $aControl surfaces.$2nasat
650 7 $aPitch (Inclination)$2nasat
650 7 $aWind tunnel tests.$2nasat
700 1 $aWalker, Charlotte E.
710 2 $aLangley Research Center.
830 0 $aNASA technical memorandum$v209104..
852 30 $aMChB$bGOV$cFICHE$hNAS 1.15:209104$91
948 $aLTI 08/08/2000