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Analysis of internal flows relative to the space shuttle main engine [[electronic resource] ] : final report
Analysis of internal flows relative to the space shuttle main engine [[electronic resource] ] : final report
Pubbl/distr/stampa Huntsville, AL : , : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center
Descrizione fisica 1 volume
Collana NASA-CR
Soggetto topico Computational fluid dynamics
Space Shuttle Main Engine
Turbulent flow
Two phase flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Analysis of internal flows relative to the space shuttle main engine
Record Nr. UNINA-9910698881703321
Huntsville, AL : , : Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Application of laser velocimetry to unsteady flows in large scale high speed tunnels / / F.K. Owen
Application of laser velocimetry to unsteady flows in large scale high speed tunnels / / F.K. Owen
Autore Owen F. Kevin
Pubbl/distr/stampa Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , [1983?]
Descrizione fisica 1 online resource (14 pages) : illustrations
Collana NASA/CR
Soggetto topico Laser applications
Flow distribution
Transonic wind tunnels
Flow velocity
Turbulent flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709660103321
Owen F. Kevin  
Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , [1983?]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor / / G. James Van Fossen, Ronald S. Bunker
Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor / / G. James Van Fossen, Ronald S. Bunker
Autore VanFossen G. James
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2000
Descrizione fisica 1 online resource (9 pages) : illustrations
Collana NASA/TM
Soggetto topico Augmentation
Stagnation point
Flow distribution
Heat transfer
Gas turbines
Turbulent flow
Isotropic turbulence
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Augmentation of stagnation region heat transfer due to turbulence from a Dry-Low-NOx can combustor
Record Nr. UNINA-9910706214703321
VanFossen G. James  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2000
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Calculation of reattaching shear layers in divergent channel with a multiple-time-scale turbulence model [[electronic resource] /] / S.-W. Kim
Calculation of reattaching shear layers in divergent channel with a multiple-time-scale turbulence model [[electronic resource] /] / S.-W. Kim
Autore Kim S. W
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration
Descrizione fisica 25 pages : digital, PDF file
Collana NASA technical memorandum
Soggetto topico Channel flow
Reattached flow
Shear layers
Turbulence models
Turbulent flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910697913903321
Kim S. W  
[Washington, D.C.] : , : National Aeronautics and Space Administration
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Calculation of turbulence-driven secondary motion in ducts with arbitrary cross section [[electronic resource] /] / A.O. Demuren
Calculation of turbulence-driven secondary motion in ducts with arbitrary cross section [[electronic resource] /] / A.O. Demuren
Autore Demuren A. O
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration
Descrizione fisica 19 pages : digital, PDF file
Collana NASA technical memorandum
Soggetto topico Computational fluid dynamics
Ducts
Finite volume method
Reynolds stress
Turbulence models
Turbulent flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910697903103321
Demuren A. O  
[Washington, D.C.] : , : National Aeronautics and Space Administration
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / / David O. Davis
CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / / David O. Davis
Autore Davis David O.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015
Descrizione fisica 1 online resource (13 pages) : color illustrations
Collana NASA/TM
Soggetto topico Boundary layers
Computational fluid dynamics
Shock wave interaction
Flow measurement
Turbulent flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction
Record Nr. UNINA-9910704277603321
Davis David O.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015
Materiale a stampa
Lo trovi qui: Univ. Federico II
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CFD vision 2030 study : a path to revolutionary computational aerosciences / / Jeffrey Slotnick [and six others]
CFD vision 2030 study : a path to revolutionary computational aerosciences / / Jeffrey Slotnick [and six others]
Autore Slotnick Jeffrey
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2014
Descrizione fisica 1 online resource (ii, 51 pages) : illustrations
Collana NASA-CR
Soggetto topico Aerospace sciences
Computational fluid dynamics
Aerothermodynamics
Transition flow
Turbulent flow
Separated flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti CFD vision 2030 study
Record Nr. UNINA-9910702577403321
Slotnick Jeffrey  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Comparing spray characteristics from Reynolds Averaged Navier-Stokes (RANS) National Combustion Code (NCC) calculations against experimental data for a turbulent reacting flow [[electronic resource] /] / Anthony C. Iannetti and Jeffery P. Moder ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 4-7, 2010
Comparing spray characteristics from Reynolds Averaged Navier-Stokes (RANS) National Combustion Code (NCC) calculations against experimental data for a turbulent reacting flow [[electronic resource] /] / Anthony C. Iannetti and Jeffery P. Moder ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 4-7, 2010
Autore Iannetti Anthony C
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica 1 online resource (v, 39 pages) : illustrations
Altri autori (Persone) ModerJeffrey P
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Turbulent flow
Spray characteristics
Jet engine fuels
Reaction kinetics
Hydrocarbons
Sulfur dioxides
Nitrogen oxides
Exhaust emission
Fuel injection
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Comparing spray characteristics from Reynolds Averaged Navier-Stokes
Record Nr. UNINA-9910699641303321
Iannetti Anthony C  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Convergence analysis of turbulent flow solutions / / Harold L. Atkins
Convergence analysis of turbulent flow solutions / / Harold L. Atkins
Autore Atkins Harold
Pubbl/distr/stampa Hampton, VA : , : National Aeronautics and Space Administration, NASA Langley Research Center, , October 2018
Descrizione fisica 1 online resource (39 pages) : illustrations
Collana NASA/TM
Soggetto topico Turbulent flow
Convergence
Computational fluid dynamics
Flow equations
Aerodynamic coefficients
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910711660503321
Atkins Harold  
Hampton, VA : , : National Aeronautics and Space Administration, NASA Langley Research Center, , October 2018
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Critical assessment of Reynolds stress turbulence models using homogeneous flows [[electronic resource] /] / Aamir Shabbir and Tsan-Hsing Shih
Critical assessment of Reynolds stress turbulence models using homogeneous flows [[electronic resource] /] / Aamir Shabbir and Tsan-Hsing Shih
Autore Shabbir Aamir
Pubbl/distr/stampa Cleveland, Ohio : , : Lewis Research Center, Institute for Computational Mechanics in Propulsion, Center for Modeling of Turbulence and Transition, , [1992]
Descrizione fisica 1 online resource (29 pages) : digital, PDF file
Altri autori (Persone) ShihTsan-Hsing <1940->
Collana NASA technical memorandum
Soggetto topico Computational fluid dynamics
Reynolds stress
Turbulence models
Turbulent flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699533703321
Shabbir Aamir  
Cleveland, Ohio : , : Lewis Research Center, Institute for Computational Mechanics in Propulsion, Center for Modeling of Turbulence and Transition, , [1992]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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