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100   $a20170614d1996      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTransonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method /$fJohn W. Edwards
210  1$a[Washington, DC] :$c[National Aeronautics and Space Administration],$d[1996]
215   $a1 online resource (16 pages) $cillustrations
225 1 $aNASA-TM ;$v110484
300   $a"EUROMECH-ColIoquium 349 Simulation of Fluid-Structure Interaction in Aeronautics, Gottingen, Germany, September 16-18, 1996."
320   $aIncludes bibliographical references (pages 15-16).
606   $aSeparated flow$2nasat
606   $aTransonic flow$2nasat
606   $aTransonic flutter$2nasat
606   $aTransonic speed$2nasat
606   $aUnsteady flow$2nasat
606   $aViscous flow$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aCoupling$2nasat
606   $aAirfoils$2nasat
606   $aMach number$2nasat
606   $aBoundary layer separation$2nasat
606   $aAirfoil oscillations$2nasat
615  7$aSeparated flow.
615  7$aTransonic flow.
615  7$aTransonic flutter.
615  7$aTransonic speed.
615  7$aUnsteady flow.
615  7$aViscous flow.
615  7$aComputational fluid dynamics.
615  7$aCoupling.
615  7$aAirfoils.
615  7$aMach number.
615  7$aBoundary layer separation.
615  7$aAirfoil oscillations.
700   $aEdwards$b John W.$0684
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705776803321
996   $aTransonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method$93533199
997   $aUNINA