LEADER 01793nam  2200481   450 
001 9910707012003321
005 20160906145346.0
035   $a(CKB)5470000002461372
035   $a(OCoLC)945978511
035   $a(EXLCZ)995470000002461372
100   $a20160405j199602    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges /$fJulio Chu and James M. Luckring
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dFebruary 1996.
215   $a1 online resource (4 volumes) $cillustrations
225 1 $aNASA technical memorandum ;$v4645
300   $aTitle from title screen (viewed April 5, 2016).
300   $a"February 1996."
320   $aIncludes bibliographical references.
327   $av. 1. Sharp leading edge -- v. 2. Small-radius leading edge -- v. 3 Medium-radius leading edge -- v. 4 Large-radius leading edge.
606   $aDelta wings$2nasat
606   $aMach number$2nasat
606   $aReynolds number$2nasat
606   $aWind tunnel tests$2nasat
606   $aLeading edges$2nasat
615  7$aDelta wings.
615  7$aMach number.
615  7$aReynolds number.
615  7$aWind tunnel tests.
615  7$aLeading edges.
700   $aChu$b Julio$01412270
702   $aLuckring$b James M.
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707012003321
996   $aExperimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges$93505269
997   $aUNINA