LEADER 01248nam a2200313 i 4500
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008 980410s1996    uk            ||| | eng  
020   $a0582035392
035   $ab10835076-39ule_inst
035   $aLE01310907$9ExL
040   $aDip.to Matematica$beng
082 0 $a515.353
084   $aAMS 35J15
100 1 $aVeron, Laurent$055416
245 10$aSingularities of solutions of second order quasilinear equations /$cLaurent Véron
260   $aHarlow, Essex, England :$bLongman,$c1996
300   $a377 p. ;$c25 cm.
490 0 $aPitman research notes in mathematics series, ISSN 02693674 ;$v353
650  4$aElliptic differential equations-numerical solutions
650  4$aNonlinear differential equations-numerical solutions
650  4$aParabolic differential equations-numerical solutions
650  4$aSingularities
907   $a.b10835076$b23-02-17$c28-06-02
912   $a991001348189707536
945   $aLE013 35J VER11 (1996)$g1$i2013000097435$lle013$o-$pE0.00$q-$rl$s-  $t0$u0$v0$w0$x0$y.i10944473$z28-06-02
996   $aSingularities of solutions of second order quasilinear equations$9345564
997   $aUNISALENTO
998   $ale013$b01-01-98$cm$da  $e-$feng$guk $h0$i1

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100   $a20110107d2010      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEstimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods$b[electronic resource] /$fGary E. Erickson
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2010]
215   $a1 online resource (v, 36 pages) $cillustrations
225 1 $aNASA/TM- ;$v2010-216196
300   $aTitle from title screen (viewed on Jan. 7, 2011).
300   $a"February 2010."
320   $aIncludes bibliographical references (pages 23-24).
410  0$aNASA technical memorandum ;$v216196.
606   $aAerodynamic characteristics$2nasat
606   $aControl surfaces$2nasat
606   $aLaunch vehicles$2nasat
606   $aShock wave interaction$2nasat
606   $aSupersonic speed$2nasat
615  7$aAerodynamic characteristics.
615  7$aControl surfaces.
615  7$aLaunch vehicles.
615  7$aShock wave interaction.
615  7$aSupersonic speed.
700   $aErickson$b Gary E$01403144
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697041703321
996   $aEstimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods$93519399
997   $aUNINA