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035   $aPARLA187641$9ExL
040   $aDip.to Filosofia$bita
082 0 $a301.32
100 1 $aClark, Colin$0120279
245 13$aIl mito dell'esplosione demografica /$cColin Clark ; prefazione di Cesare Zappulli
260   $aMilano :$bAres,$c1974
300   $a188 p. ;$c20 cm.
490 0 $aCollana Faretra ;$v1
500   $aTrad. R. Arduini
650  4$aPopolazione - Aumento
650  4$aRisorse naturali$xUtilizzazione
700 1 $aArduini, Renato
740 4 $aThe myth of over-population
907   $a.b11207243$b23-02-17$c01-07-02
912   $a991003737789707536
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996   $aMito dell'esplosione demografica$9870414
997   $aUNISALENTO
998   $ale005$b01-01-99$cm$da  $e-$fita$git $h3$i1

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100   $a20170208j201611    ua         0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFull-field reconstruction of structural deformations and loads from measured strain data on a wing test article using the inverse finite element method /$fEric J. Miller and Russel Manalo, Alexander Tessler
210  1$aEdwards, California :$cNational Aeronautics and Space Administration, Armstrong Flight Research Center,$dNovember 2016.
215   $a1 online resource (29 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2016-219407
300   $a"November 2016."
320   $aIncludes bibliographical references (pages 28-29).
606   $aAerodynamic loads$2nasat
606   $aBody-wing and tail configurations$2nasat
606   $aDeformation$2nasat
606   $aFinite element method$2nasat
606   $aStrain measurement$2nasat
606   $aWing loading$2nasat
615  7$aAerodynamic loads.
615  7$aBody-wing and tail configurations.
615  7$aDeformation.
615  7$aFinite element method.
615  7$aStrain measurement.
615  7$aWing loading.
700   $aMiller$b Eric J.$0614271
702   $aManalo$b Russel
702   $aTessler$b Alexander
712 02$aNASA Neil A. Armstrong Flight Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707942003321
996   $aFull-field reconstruction of structural deformations and loads from measured strain data on a wing test article using the inverse finite element method$93465795
997   $aUNINA