LEADER 01925nam  2200481   450 
001 9910704382503321
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035   $a(CKB)5470000002439857
035   $a(OCoLC)942651780
035   $a(EXLCZ)995470000002439857
100   $a20160302j199612    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSurface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber /$fS. Naomi McMillin [and five others]
210  1$aHampton, VA :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1996.
215   $a1 online resource (iii, 262 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4673
300   $aTitle from title screen (viewed March 2, 2016).
300   $a"December 1996."
300   $a"Performing organization: NASA Langley Research Center, Hampton, VA"--Report documentation page.
320   $aIncludes bibliographical references (page 262).
606   $aDelta wings$2nasat
606   $aFlow visualization$2nasat
606   $aLeading edges$2nasat
606   $aReynolds number$2nasat
606   $aBoundary layer transition$2nasat
615  7$aDelta wings.
615  7$aFlow visualization.
615  7$aLeading edges.
615  7$aReynolds number.
615  7$aBoundary layer transition.
700   $aMcMillin$b S. Naomi$g(Susan Naomi),$01419322
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704382503321
996   $aSurface-pressure and flow-visualization data at Mach number of 1.60 for three 65° delta wings varying in leading-edge radius and camber$93533368
997   $aUNINA