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Factors influencing pitot probe centerline displacement in a turbulent supersonic boundary layer / / Wendy I. Grosser
Factors influencing pitot probe centerline displacement in a turbulent supersonic boundary layer / / Wendy I. Grosser
Autore Grosser Wendy I.
Pubbl/distr/stampa Cleveland, Ohio : , : National National Aeronautics and Space Administration, Lewis Research Center, , January1997
Descrizione fisica 1 online resource (46 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Pressure sensors
Supersonic flow
Turbulent flow
Wind tunnel tests
Turbulent boundary layer
Reynolds number
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707328703321
Grosser Wendy I.  
Cleveland, Ohio : , : National National Aeronautics and Space Administration, Lewis Research Center, , January1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Final report for NASA Ames cooperative agreement, NCC2-5049
Final report for NASA Ames cooperative agreement, NCC2-5049
Pubbl/distr/stampa [Davis, Calif.] : , : Department of Mechanical and Aeronautical Engineering, University of California, Davis, , 1996
Descrizione fisica 1 online resource (7 pages) : illustrations
Collana [NASA contractor report]
Soggetto topico Convergence
Mathematical optimization
Supersonic flow
Transonic flow
Optimization
Design analysis
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Optimum shape design using automatic differentiation in reverse mode
Record Nr. UNINA-9910707158803321
[Davis, Calif.] : , : Department of Mechanical and Aeronautical Engineering, University of California, Davis, , 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Flow matching results of an MHD energy bypass system on a supersonic turbojet engine using the numerical propulsion system simulation (NPSS) environment [[electronic resource] /] / Theresa L. Benyo
Flow matching results of an MHD energy bypass system on a supersonic turbojet engine using the numerical propulsion system simulation (NPSS) environment [[electronic resource] /] / Theresa L. Benyo
Autore Benyo Theresa L
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Descrizione fisica 1 online resource (14 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Propulsion system performance
Turbojet engines
Energy technology
Magnetohydrodynamic generators
Systems simulation
Bypasses
Supersonic flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Flow matching results of an MHD energy bypass system on a supersonic turbojet engine using the numerical propulsion system simulation
Record Nr. UNINA-9910701469303321
Benyo Theresa 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
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
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Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport / / Milton Lamb, John R. Carlson, and Odis C. Pendergraft
Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport / / Milton Lamb, John R. Carlson, and Odis C. Pendergraft
Autore Lamb Milton
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , November 1987
Descrizione fisica 1 online resource (21 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Angle of attack
Nacelles
Separated flow
Supersonic flow
Transonic wind tunnels
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707804103321
Lamb Milton  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , November 1987
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Investigation of flow separation in a transonic-fan linear cascade using visualization methods / / Jan Lepicovsky [and four others]
Investigation of flow separation in a transonic-fan linear cascade using visualization methods / / Jan Lepicovsky [and four others]
Autore Lepicovsky Jan
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2000
Descrizione fisica 1 online resource (13 pages) : illustrations
Collana NASA/TM
Soggetto topico Transonic flutter
Flow visualization
Supersonic flow
Boundary layer separation
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706207503321
Lepicovsky Jan  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2000
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The Kirchhoff formulas for moving surfaces in aeroacoustics: the subsonic and supersonic cases / / F. Farassat
The Kirchhoff formulas for moving surfaces in aeroacoustics: the subsonic and supersonic cases / / F. Farassat
Autore Farassat F.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1996
Descrizione fisica 1 online resource (111 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Kirchhoff law
Pipe flow
Subsonic speed
Aeroacoustics
Electromagnetism
Supersonic flow
Noise prediction
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Kirchhoff formulas for moving surfaces in aeroacoustics
Record Nr. UNINA-9910707912903321
Farassat F.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors / / Andreja Brankovic [and nine others]
Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors / / Andreja Brankovic [and nine others]
Autore Brankovic Andreja
Pubbl/distr/stampa Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2002
Descrizione fisica 1 online resource (41 pages) : illustrations
Collana NASA/TM
Soggetto topico Combustion chambers
Lobe mixer
Supersonic flow
Pitot tubes
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910708614403321
Brankovic Andreja  
Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2002
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
NASA Glenn 1-by 1-foot supersonic wind tunnel user manual / / Kirk D. Seablom [and four others]
NASA Glenn 1-by 1-foot supersonic wind tunnel user manual / / Kirk D. Seablom [and four others]
Autore Seablom Kirk D.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 1999
Descrizione fisica 1 online resource (iv, 46 pages) : illustrations
Collana NASA/TM
Soggetto topico Mach number
Reynolds number
Supersonic wind tunnels
Supersonic flow
Test chambers
Data acquisition
Manuals
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti NASA Glenn one by one foot supersonic wind tunnel user manual
Record Nr. UNINA-9910706185103321
Seablom Kirk D.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 1999
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Photodiagnostics of turbulent flows using laser-induced fluorescence : final report / / Daniel Bershader
Photodiagnostics of turbulent flows using laser-induced fluorescence : final report / / Daniel Bershader
Autore Bershader Daniel
Pubbl/distr/stampa Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , December 1983
Descrizione fisica 1 online resource (various pagings) : illustrations
Collana NASA/CR
Soggetto topico Turbulent flow
Supersonic flow
Boundary layer flow
Laser applications
Temperature gradients
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Photodiagnostics of turbulent flows using laser-induced fluorescence
Record Nr. UNINA-9910709832903321
Bershader Daniel  
Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , December 1983
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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