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Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design / / David J. Friedlander, Christopher M. Heath, and Raymond S. Castner
Numerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design / / David J. Friedlander, Christopher M. Heath, and Raymond S. Castner
Autore Friedlander David J.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2018
Descrizione fisica 1 online resource (55 pages) : color illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Supersonic aircraft
Reynolds averaging
Grid refinement (mathematics)
Computerized simulation
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Numerical simulations of a Quiet SuperSonic Technology
Record Nr. UNINA-9910711552903321
Friedlander David J.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2018
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Reynolds-averaged Navier-Stokes solutions to flat plate film cooling scenarios [[electronic resource] /] / Perry L. Johnson, Vikram Shyam and Chunill Hah
Reynolds-averaged Navier-Stokes solutions to flat plate film cooling scenarios [[electronic resource] /] / Perry L. Johnson, Vikram Shyam and Chunill Hah
Autore Johnson Perry L
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Descrizione fisica 1 online resource (21 pages) : color illustrations
Altri autori (Persone) ShyamVikram
HahC
Collana NASA/TM
Soggetto topico Film cooling
Flat plates
Navier-Stokes equation
Reynolds averaging
Mathematical models
Grid refinement (mathematics)
Gas turbine engines
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701152503321
Johnson Perry L  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Updates to simulation of a single-element lean-direct injection combustor using a polyhedral mesh derived from hanging-node elements / / Changju Thomas Wey and Nan-Suey Liu
Updates to simulation of a single-element lean-direct injection combustor using a polyhedral mesh derived from hanging-node elements / / Changju Thomas Wey and Nan-Suey Liu
Autore Wey Changju Thomas
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2014
Descrizione fisica 1 online resource (14 pages) : color illustrations
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Navier-Stokes equation
Grid generation (mathematics)
Large eddy simulation
Grid refinement (mathematics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910703640203321
Wey Changju Thomas  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , March 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui