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200 1 $a<<La>> guida di Peter Norton a l'hardware dei PC$fPeter Norton, Michael Desmond$g[traduzione di Clara Mengolini]
210   $aMilano$cApogeo$dcopyr. 1999
215   $aXXV, 773 p.$cill.$d24 cm
312   $aTrad. di: peter norton's complete guide to pc upgrades
610 1 $aelaboratori elettronici
610 1 $ahardware
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702  1$aDesmond,$bMichael
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979   $aPATRY$b90$c20040406$lUSA01$h1618
996   $aGuida di Peter Norton a l'hardware dei PC$91502418
997   $aUNISA

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100   $a20131018d2013      ua             0
101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 10$aWind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds /$fGary E. Erickson
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2013]
215   $a1 online resource (521 pages) $cillustrations
225 1 $aNASA/TM 2013-217982
300   $aTitle from title screen (viewed Oct. 18, 2013).
300   $a"April 2013."
320   $aIncludes bibliographical references (page 41).
606   $aLeading edges$2nasat
606   $aAerodynamic configurations$2nasat
606   $aAngle of attack$2nasat
606   $aCanard configurations$2nasat
606   $aFlow visualization$2nasat
606   $aSubsonic speed$2nasat
606   $aPorosity$2nasat
606   $aTransonic speed$2nasat
606   $aVortices$2nasat
606   $aReynolds number$2nasat
606   $aMach number$2nasat
615  7$aLeading edges.
615  7$aAerodynamic configurations.
615  7$aAngle of attack.
615  7$aCanard configurations.
615  7$aFlow visualization.
615  7$aSubsonic speed.
615  7$aPorosity.
615  7$aTransonic speed.
615  7$aVortices.
615  7$aReynolds number.
615  7$aMach number.
700   $aErickson$b Gary E.$01403144
712 02$aUnited States.$bNational Aeronautics and Space Administration,
712 02$aLangley Research Center,
801  0$bGPO
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