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200 1 $aSecure transaction protocol analysis$emodels and applications$fQingfeng Chen, Chengqi Zhang, Shichao Zhang
210   $aBerlin$cSpringer$dcopyr. 2008
215   $aXI, 234 p.$d24 cm
225 2 $aLecture notes in computer science$v5111
410  0$12001$aLecture notes in computer science
461  1$10010003149690$12001$aLecture notes in computer science$12001
606 0 $aSicurezza del computer
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700  1$aCHEN,$bQingfeng$0508840
701  1$aZHANG,$bChengqi$0497864
701  1$aZHANG,$bShichao$0497865
801  0$aIT$bsalbc$gISBD
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979   $aCBAS$b10$c20080929$lUSA01$h1049
996   $aSecure Transaction Protocol Analysis$9774452
997   $aUNISA

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100   $a20141126j201401    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aActive vibration control for helicopter interior noise reduction using power minimization /$fJ. Mendoza [and four others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJanuary 2014.
215   $a1 online resource (197 pages) $ccolor illustrations
225 1 $aNASA-CR ;$v2014-218147
300   $aTitle from title screen (viewed Nov. 26, 2014).
300   $a"January 2014."
320   $aIncludes bibliographical references (pages 187-191).
606   $aNoise reduction$2nasat
606   $aRotary wing aircraft$2nasat
606   $aAircraft compartments$2nasat
606   $aOptimal control$2nasat
606   $aStructural vibration$2nasat
606   $aVibration damping$2nasat
615  7$aNoise reduction.
615  7$aRotary wing aircraft.
615  7$aAircraft compartments.
615  7$aOptimal control.
615  7$aStructural vibration.
615  7$aVibration damping.
700   $aMendoza$b J.$0171843
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702574903321
996   $aActive vibration control for helicopter interior noise reduction using power minimization$93522951
997   $aUNINA