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An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization / / Erik L. Axdahl
An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization / / Erik L. Axdahl
Autore Axdahl Erik L.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015
Descrizione fisica 1 online resource (31 pages) : color illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Design optimization
Supersonic nozzles
Numerical analysis
Test facilities
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Automated design analysis kit for optimization and terascale applications and viscous upwind algorithm for complex flow analysis computational fluid dynamics framework with application to supersonic facility nozzle flowpath optimization
Record Nr. UNINA-9910704019103321
Axdahl Erik L.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015
Materiale a stampa
Lo trovi qui: Univ. Federico II
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An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code / / Mary Ann Dembowski and Nicholas J. Georgiadis
An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code / / Mary Ann Dembowski and Nicholas J. Georgiadis
Autore Dembowski Mary Ann
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2002
Descrizione fisica 1 online resource (18 pages) : illustrations
Collana NASA/TM
Soggetto topico Jet mixing flow
Navier-Stokes equation
Nozzle flow
Turbulence models
Turbulent mixing
Supersonic nozzles
Applications programs (computers)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705682203321
Dembowski Mary Ann  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2002
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0 / / by Robert J. McGhee and James A. Martin
Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0 / / by Robert J. McGhee and James A. Martin
Autore McGhee Robert J.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969
Descrizione fisica 1 online resource (39 pages) : illustrations
Collana NASA technical note
Soggetto topico Aerodynamics, Supersonic
Supersonic nozzles
Mach number
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910714046903321
McGhee Robert J.  
Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui