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035   $aLE01303949$9ExL
040   $aDip.to Matematica$beng
082 0 $a511.3
084   $aAMS 03B52
084   $aQA76.87.N497
100 1 $aNguyen, Hung T.$0117426
245 12$aA first course in fuzzy logic /$cHung T. Nguyen, Elbert A. Walker
250   $a2nd ed
260   $aBoca Raton, FL :$bChapman & Hall,$cc2000
300   $a373 p. :$bill. ;$c24 cm.
500   $aIncludes bibliographical references (p. 335-349)
650  4$aFuzzy logic
650  4$aNeural networks (Computer science)
700 1 $aWalker, Elbert A.
907   $a.b10772212$b21-09-06$c28-06-02
912   $a991000893919707536
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996   $aFirst course in fuzzy logic$9207945
997   $aUNISALENTO
998   $ale013$b01-01-01$cm$da  $e-$feng$gus $h2$i1

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100   $a20150604j201502    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEnabling rapid and robust structural analysis during conceptual design /$fLloyd B. Eldred, Sharon L. Padula, and Wu Li
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dFebruary 2015.
215   $a1 online resource (21 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218687
300   $aTitle from title screen (viewed June 4, 2015).
300   $a"February 2015."
320   $aIncludes bibliographical references (pages 20-21).
606   $aStructural analysis$2nasat
606   $aAerodynamic loads$2nasat
606   $aSupersonic aircraft$2nasat
606   $aBody-wing configurations$2nasat
606   $aDesign analysis$2nasat
615  7$aStructural analysis.
615  7$aAerodynamic loads.
615  7$aSupersonic aircraft.
615  7$aBody-wing configurations.
615  7$aDesign analysis.
700   $aEldred$b Lloyd B.$01408898
702   $aPadula$b S. L.
702   $aLi$b Wu
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703786703321
996   $aEnabling rapid and robust structural analysis during conceptual design$93494011
997   $aUNINA