LEADER 01876nam  2200529 a 450 
001 9910701851103321
005 20120618080714.0
035   $a(CKB)5470000002421597
035   $a(OCoLC)795702130
035   $a(EXLCZ)995470000002421597
100   $a20120618d2011      ua             0
101 0 $aeng
135   $aurmn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aUnsteady aerodynamic model tuning for precise flutter prediction$b[electronic resource] /$fChan-gi Pak
210  1$aEdwards, CA :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$d[2011]
215   $a1 online resource (18 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2011-215963
300   $aTitle from title screen (viewed on June 18, 2012).
300   $a"April 2011."
320   $aIncludes bibliographical references (pages 17-18).
606   $aAerodynamic coefficients$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aAeroelasticity$2nasat
606   $aFlight tests$2nasat
606   $aFlutter analysis$2nasat
606   $aInfluence coefficient$2nasat
606   $aPrediction analysis techniques$2nasat
606   $aUnsteady aerodynamics$2nasat
615  7$aAerodynamic coefficients.
615  7$aAerodynamic characteristics.
615  7$aAeroelasticity.
615  7$aFlight tests.
615  7$aFlutter analysis.
615  7$aInfluence coefficient.
615  7$aPrediction analysis techniques.
615  7$aUnsteady aerodynamics.
700   $aPak$b Chan-gi$f1956-$01395872
712 02$aHugh L. Dryden Flight Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701851103321
996   $aUnsteady aerodynamic model tuning for precise flutter prediction$93479763
997   $aUNINA