01966nam 2200505 450 991070657760332120171117135335.0(CKB)5470000002456669(OCoLC)1012121478(EXLCZ)99547000000245666920171117j200107 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierSimulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral /Max Kandula, Raoul CaimiKennedy Space Center, Florida :National Aeronautics and Space Administration, John F. Kennedy Space Center,July 2001.1 online resource (v, 18 pages) illustrationsNASA/TM ;2001-210263"July 2001"."Performing organization: NASA John F. Kennedy Space Center"--Report documentation page.Includes bibliographical references (pages 8-9).Simulation of supersonic jet noise with the adaptation of overflow Computational Fluid Dynamics code and Kirchhoff surface integralComputational fluid dynamicsnasatFlow distributionnasatGas jetsnasatJet aircraft noisenasatMathematical modelsnasatSupersonic jet flownasatComputational fluid dynamics.Flow distribution.Gas jets.Jet aircraft noise.Mathematical models.Supersonic jet flow.Kandula Max1399273Caimi Raoul E.John F. Kennedy Space Center,GPOGPOBOOK9910706577603321Simulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integral3501313UNINA