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100   $a20120408j198709    ua             0
101 0 $aeng
135   $aurbn||||||abp
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCalculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment /$fJames T. Howlett and Samuel R. Bland
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Office,$dSeptember 1987.
215   $a1 online resource (74 pages) $cillustrations
225 1 $aNASA/TP ;$v2731
300   $a"September 1987."
300   $aPrepared at Langley Research Center.
320   $aIncludes bibliographical references (page 13).
606   $aTransonic flow$2nasat
606   $aViscous flow$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aAirfoils$2nasat
606   $aOscillations$2nasat
606   $aAerodynamics, Transonic
606   $aViscous flow
606   $aUnsteady flow (Aerodynamics)
606   $aOscillating wings (Aerodynamics)
606   $aBoundary layer
606   $aAerodynamics, Transonic$2fast
606   $aBoundary layer$2fast
606   $aOscillating wings (Aerodynamics)$2fast
606   $aUnsteady flow (Aerodynamics)$2fast
606   $aViscous flow$2fast
615  7$aTransonic flow.
615  7$aViscous flow.
615  7$aComputational fluid dynamics.
615  7$aAirfoils.
615  7$aOscillations.
615  0$aAerodynamics, Transonic.
615  0$aViscous flow.
615  0$aUnsteady flow (Aerodynamics)
615  0$aOscillating wings (Aerodynamics)
615  0$aBoundary layer.
615  7$aAerodynamics, Transonic.
615  7$aBoundary layer.
615  7$aOscillating wings (Aerodynamics)
615  7$aUnsteady flow (Aerodynamics)
615  7$aViscous flow.
700   $aHowlett$b James T.$01405307
702   $aBland$b Samuel R.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910709895003321
996   $aCalculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment$93481515
997   $aUNINA