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Aerodynamic measurements of a variable-speed power-turbine blade section in a transonic turbine cascade / / Ashlie B. Flegel
Aerodynamic measurements of a variable-speed power-turbine blade section in a transonic turbine cascade / / Ashlie B. Flegel
Autore Flegel Ashlie B.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2014
Descrizione fisica 1 online resource (iv, 36 pages) : color illustrations
Collana NASA/TM
Soggetto topico Reynolds number
Turbine blades
Rotor blades (turbomachinery)
Tilt rotor aircraft
Three dimensional flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910703642403321
Flegel Ashlie B.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Development of ROT22 [[electronic resource] ] : DATAMAP interface / / K. R. Shenoy, T. Waak, J. T. Brieger
Development of ROT22 [[electronic resource] ] : DATAMAP interface / / K. R. Shenoy, T. Waak, J. T. Brieger
Autore Shenoy K. R
Pubbl/distr/stampa Moffett Field, Calif. : , : National Aeronautics and Space Administration, Ames Research Center, , [1986]
Descrizione fisica 1 online resource (xiv, 92 pages) : illustrations
Altri autori (Persone) WaakT
BriegerJ. T
Collana NASA contractor report
Soggetto topico Computer programs
Interfaces
Numerical analysis
Predictions
Rotary wings
Three dimensional flow
Transonic flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Development of ROT22
Record Nr. UNINA-9910701461703321
Shenoy K. R  
Moffett Field, Calif. : , : National Aeronautics and Space Administration, Ames Research Center, , [1986]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Development of three-dimensional DRAGON grid technology / / Yao Zheng, Meng-Sing Liou and Kestutis C. Civinskas
Development of three-dimensional DRAGON grid technology / / Yao Zheng, Meng-Sing Liou and Kestutis C. Civinskas
Autore Zheng Yao
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 1999
Descrizione fisica 1 online resource (35 pages) : illustrations
Collana NASA/TM
Soggetto topico Three dimensional flow
Structured grids (mathematics)
Computational fluid dynamics
Design analysis
Computer programs
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Development of three-dimensional Direct Replacement of Arbitrary Grid Overlapping by Nonstructured grid technology
Record Nr. UNINA-9910706147303321
Zheng Yao  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , November 1999
Materiale a stampa
Lo trovi qui: Univ. Federico II
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A dual potential formulation of the Navier-Stokes equations / / S.G. Gegg, R.H. Pletcher, J.L. Steger
A dual potential formulation of the Navier-Stokes equations / / S.G. Gegg, R.H. Pletcher, J.L. Steger
Autore Gegg S. G.
Pubbl/distr/stampa [Ames, Iowa ] : , : Heat Transfer Laboratory, Engineering Research Institute, Iowa State University
Descrizione fisica 1 online resource (xiii, 204 pages) : illustrations
Collana [NASA contractor report
Soggetto topico Compressible flow
Computational fluid dynamics
Flow velocity
Incompressible flow
Navier-Stokes equation
Poisson equation
Three dimensional flow
Two dimensional flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705372603321
Gegg S. G.  
[Ames, Iowa ] : , : Heat Transfer Laboratory, Engineering Research Institute, Iowa State University
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Dynamic stall suppression using combustion-powered actuation (COMPACT) / / Claude G. Matalanis [and nine others]
Dynamic stall suppression using combustion-powered actuation (COMPACT) / / Claude G. Matalanis [and nine others]
Autore Matalanis Claude G.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2016
Descrizione fisica 1 online resource (614 pages) : color illustrations
Collana NASA/CR
Soggetto topico Aerodynamic stalling
Computational fluid dynamics
Rotary wing aircraft
Two dimensional flow
Three dimensional flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Dynamic stall suppression using combustion-powered actuation
Record Nr. UNINA-9910705709103321
Matalanis Claude G.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage / / reported by M.F. Blair
The effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage / / reported by M.F. Blair
Autore Blair M. F.
Pubbl/distr/stampa East Hartford, Connecticut : , : United Technologies Research Center, , November 1991
Descrizione fisica 1 online resource (vi, 67 pages, 172 unnumbered pages) : illustrations
Collana NASA CR
Soggetto topico Aerodynamics
Gas turbines
Heat transfer
Rotors
Three dimensional flow
Turbine pumps
Turbulence models
Viscous flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910695071803321
Blair M. F.  
East Hartford, Connecticut : , : United Technologies Research Center, , November 1991
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Entropy stable wall boundary conditions for the compressible Navier-Stokes equations / / Matteo Parsani, Mark H. Carpenter, and Eric J. Nielsen
Entropy stable wall boundary conditions for the compressible Navier-Stokes equations / / Matteo Parsani, Mark H. Carpenter, and Eric J. Nielsen
Autore Parsani Matteo
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 2014
Descrizione fisica 1 online resource (47 pages) : color illustrations
Collana NASA/TM
Soggetto topico Navier-Stokes equation
Galerkin method
Supersonic flow
Three dimensional flow
Finite element method
Finite volume method
Finite difference theory
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702739303321
Parsani Matteo  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , June 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade / / Ali A. Ameri
Implementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade / / Ali A. Ameri
Autore Ameri Ali A.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Descrizione fisica 1 online resource (25 pages) : illustrations
Collana [NASA contractor report]
Soggetto topico Computational fluid dynamics
Turbulent boundary layer
Turbine blades
Heat transfer
Losses
Low Reynolds number
Pressure ratio
Three dimensional flow
Laminar flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702113803321
Ameri Ali A.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Inflow/outflow boundary conditions with application to FUN3D [[electronic resource] /] / Jan-Reneé Carlson
Inflow/outflow boundary conditions with application to FUN3D [[electronic resource] /] / Jan-Reneé Carlson
Autore Carlson Jan-Reneé
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Descrizione fisica 1 online resource (32 pages) : color illustrations
Collana NASA/TM
Soggetto topico Boundary conditions
Proving
Computer programs
Three dimensional flow
Subsonic flow
Supersonic flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701780703321
Carlson Jan-Reneé  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Numerical simulation of scramjet inlet flow fields / / Ajay Kumar
Numerical simulation of scramjet inlet flow fields / / Ajay Kumar
Autore Kumar Ajay
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1986
Descrizione fisica 1 online resource (26 pages) : illustrations
Collana NASA/TP
Soggetto topico Computational fluid dynamics
Inlet flow
Turbulent flow
Mach number
Three dimensional flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709877503321
Kumar Ajay  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , May 1986
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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