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100   $a20171117j200107    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSimulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral /$fMax Kandula, Raoul Caimi
210  1$aKennedy Space Center, Florida :$cNational Aeronautics and Space Administration, John F. Kennedy Space Center,$dJuly 2001.
215   $a1 online resource (v, 18 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210263
300   $a"July 2001".
300   $a"Performing organization: NASA John F. Kennedy Space Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 8-9).
517 3 $aSimulation of supersonic jet noise with the adaptation of overflow Computational Fluid Dynamics code and Kirchhoff surface integral
606   $aComputational fluid dynamics$2nasat
606   $aFlow distribution$2nasat
606   $aGas jets$2nasat
606   $aJet aircraft noise$2nasat
606   $aMathematical models$2nasat
606   $aSupersonic jet flow$2nasat
615  7$aComputational fluid dynamics.
615  7$aFlow distribution.
615  7$aGas jets.
615  7$aJet aircraft noise.
615  7$aMathematical models.
615  7$aSupersonic jet flow.
700   $aKandula$b Max$01399273
702   $aCaimi$b Raoul E.
712 02$aJohn F. Kennedy Space Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706577603321
996   $aSimulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral$93501313
997   $aUNINA