LEADER 01847nam  2200541Ia 450 
001 9910699916603321
005 20110825111651.0
035   $a(CKB)5470000002406794
035   $a(OCoLC)747821464
035   $a(EXLCZ)995470000002406794
100   $a20110825d2010      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplication of approximate unsteady aerodynamics for flutter analysis$b[electronic resource] /$fChan-gi Pak and Wesley W. Li
210  1$aEdwards, Calif. :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$d[2010]
215   $a1 online resource (20 pages) $cillustrations
225 1 $aNASA/TM ;$v2010-216387
300   $aTitle from title screen (viewed on Aug. 25, 2011).
300   $a"July 2010."
320   $aIncludes bibliographical references (page 20).
606   $aAerodynamic coefficients$2nasat
606   $aAerodynamics$2nasat
606   $aApproximation$2nasat
606   $aFlutter$2nasat
606   $aFlutter analysis$2nasat
606   $aPrediction analysis techniques$2nasat
606   $aUnsteady aerodynamics$2nasat
606   $aWings$2nasat
615  7$aAerodynamic coefficients.
615  7$aAerodynamics.
615  7$aApproximation.
615  7$aFlutter.
615  7$aFlutter analysis.
615  7$aPrediction analysis techniques.
615  7$aUnsteady aerodynamics.
615  7$aWings.
700   $aPak$b Chan-gi$01386346
701   $aLi$b Wesley W$01405427
712 02$aHugh L. Dryden Flight Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910699916603321
996   $aApplication of approximate unsteady aerodynamics for flutter analysis$93519791
997   $aUNINA