LEADER 02022nam  2200565 a 450 
001 9910701851203321
005 20120618083754.0
035   $a(CKB)5470000002421596
035   $a(OCoLC)795702203
035   $a(EXLCZ)995470000002421596
100   $a20120618d2011      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aBasis function approximation of transonic aerodynamic influence coefficient matrix$b[electronic resource] /$fWesley W. Li and Chan-gi Pak
210  1$aEdwards, CA :$cNational Aeronautics and Space Administration, Dryden Flight Research Center,$d[2011]
215   $a1 online resource (17 pages) $cillustrations
225 1 $aNASA/TM ;$v2011-216423
300   $aTitle from title screen (viewed on June 18, 2012).
300   $a"March 2011."
320   $aIncludes bibliographical references (page 17).
606   $aMatrices (mathematics)$2nasat
606   $aTransonic flow$2nasat
606   $aAerodynamic coefficients$2nasat
606   $aDesign optimization$2nasat
606   $aApproximation$2nasat
606   $aFlutter analysis$2nasat
606   $aInfluence coefficient$2nasat
606   $aPrediction analysis techniques$2nasat
606   $aUnsteady aerodynamics$2nasat
615  7$aMatrices (mathematics)
615  7$aTransonic flow.
615  7$aAerodynamic coefficients.
615  7$aDesign optimization.
615  7$aApproximation.
615  7$aFlutter analysis.
615  7$aInfluence coefficient.
615  7$aPrediction analysis techniques.
615  7$aUnsteady aerodynamics.
700   $aLi$b Wesley W$01405427
701   $aPak$b Chan-gi$f1956-$01395872
712 02$aHugh L. Dryden Flight Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910701851203321
996   $aBasis function approximation of transonic aerodynamic influence coefficient matrix$93481897
997   $aUNINA