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LEADER 01983nam  2200565Ia 450 
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035   $a(CKB)5470000002412894
035   $a(OCoLC)754787480
035   $a(EXLCZ)995470000002412894
100   $a20110927d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aReduced uncertainties in the flutter analysis of the aerostructures test wing$b[electronic resource] /$fChan-gi Pak and Shun-fat Lung
210  1$aEdwards, CA :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$d[2011]
215   $a1 online resource (25 pages) $cillustrations, (some color)
225 1 $aNASA/TM ;$v2011-216421
300   $aTitle from title screen (viewed on Sept. 27, 2011).
300   $a"January 2011."
320   $aIncludes bibliographical references (pages 13-14).
606   $aFlutter analysis$2nasat
606   $aDynamic structural analysis$2nasat
606   $aDesign analysis$2nasat
606   $aWings$2nasat
606   $aFinite element method$2nasat
606   $aMultidisciplinary design optimization$2nasat
606   $aFlight tests$2nasat
606   $aDynamic models$2nasat
606   $aTuning$2nasat
615  7$aFlutter analysis.
615  7$aDynamic structural analysis.
615  7$aDesign analysis.
615  7$aWings.
615  7$aFinite element method.
615  7$aMultidisciplinary design optimization.
615  7$aFlight tests.
615  7$aDynamic models.
615  7$aTuning.
700   $aPak$b Chan-gi$f1956-$01395872
701   $aLung$b Shun-fat$01395873
712 02$aHugh L. Dryden Flight Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700812703321
996   $aReduced uncertainties in the flutter analysis of the aerostructures test wing$93455056
997   $aUNINA