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14- by 22-foot subsonic tunnel laser velocimeter upgrade / / James F. Meyers [and three others]
14- by 22-foot subsonic tunnel laser velocimeter upgrade / / James F. Meyers [and three others]
Autore Meyers James F.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012
Descrizione fisica 1 online resource (793 unnumbered pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Analog to digital converters
Laser doppler velocimeters
Subsonic wind tunnels
Wind tunnel tests
Data acquisition
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Fourteen by twenty two-foot subsonic tunnel laser velocimeter upgrade
Record Nr. UNINA-9910704474203321
Meyers James F.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012
Materiale a stampa
Lo trovi qui: Univ. Federico II
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The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / / Christopher E. Hughes [and three others]
The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / / Christopher E. Hughes [and three others]
Autore Hughes Christopher E.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2013
Descrizione fisica 1 online resource (35 pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Aeroacoustics
Aerodynamic characteristics
Aerodynamic noise
Aircraft noise
Fan blades
Far fields
Laser doppler velocimeters
Low speed wind tunnels
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702436703321
Hughes Christopher E.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Evolution of a planar wake in adverse pressure gradient / / David M. Driver, George G. Mateer
Evolution of a planar wake in adverse pressure gradient / / David M. Driver, George G. Mateer
Autore Driver David M.
Pubbl/distr/stampa Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , February 2016
Descrizione fisica 1 online resource (67 pages) : color illustrations
Collana NASA/TM
Soggetto topico Laser doppler velocimeters
Pressure gradients
Reversed flow
Reynolds stress
Turbulence models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707645603321
Driver David M.  
Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , February 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight : comprehensive data report / / K. Yamamoto [and four others]
Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight : comprehensive data report / / K. Yamamoto [and four others]
Autore Yamamoto K.
Pubbl/distr/stampa Cincinnati, Ohio : , : General Electric Company, Aircraft Engine Business Group, , February, 1984
Descrizione fisica 1 online resource (2 volumes) : illustrations
Collana NASA CR
Soggetto topico Acoustic measurement
Nozzle design
Scale models
Laser doppler velocimeters
Shadowgraph photography
Static pressure
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto v. 1. Test nozzles and acoustic data -- v. 2. Laser velocimeter data, static pressures and shadowgraph photos.
Altri titoli varianti Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight
Record Nr. UNINA-9910703872603321
Yamamoto K.  
Cincinnati, Ohio : , : General Electric Company, Aircraft Engine Business Group, , February, 1984
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Fluorescence-doped particles for simultaneous temperature and velocity imaging / / Paul M. Danehy [and seven others]
Fluorescence-doped particles for simultaneous temperature and velocity imaging / / Paul M. Danehy [and seven others]
Autore Danehy Paul M.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2012]
Descrizione fisica 1 online resource (13 pages) : illustrations
Collana NASA/TM 2012-217768
Soggetto topico Microparticles
Polystyrene
Synthesis (chemistry)
Wind tunnel tests
Dyes
Particle image velocimetry
Fluorescence
Laser doppler velocimeters
Latex
Temperature measurement
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704475003321
Danehy Paul M.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2012]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The NASA subsonic jet particle image velocimetry (PIV) dataset [[electronic resource] /] / James Bridges and Mark P. Wernet
The NASA subsonic jet particle image velocimetry (PIV) dataset [[electronic resource] /] / James Bridges and Mark P. Wernet
Autore Bridges James
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Descrizione fisica 1 online resource (49 pages) : illustrations (some color)
Altri autori (Persone) WernetMark P
Collana NASA/TM
Soggetto topico Computational fluid dynamics
Gas jets
Subsonic flow
Turbulence
Particle image velocimetry
Laser doppler velocimeters
Acoustic velocity
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti NASA subsonic jet particle image velocimetry
Record Nr. UNINA-9910701572003321
Bridges James  
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
Seeding for laser velocimetry in confined supersonic flows with shocks / / J. Lepicovsky and RJ. Bruckner
Seeding for laser velocimetry in confined supersonic flows with shocks / / J. Lepicovsky and RJ. Bruckner
Autore Lepicovsky Jan
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1996
Descrizione fisica 1 online resource (9 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Laser doppler velocimeters
Reliability
Supersonic flow
Optical measuring instruments
Velocity measurement
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707356503321
Lepicovsky Jan  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Study of high-speed combustion flows by laser velocimetry [[electronic resource] /] / H. J. Schaefer
Study of high-speed combustion flows by laser velocimetry [[electronic resource] /] / H. J. Schaefer
Autore Schaefer H. J
Pubbl/distr/stampa Saint-Louis, France : , : [Insitut Franco-Allemand de Recherches]
Descrizione fisica 1 online resource (29 unnumbered pages) : illustrations
Collana [NASA CR
Soggetto topico Flow velocity
Laser doppler velocimeters
Supersonic combustion
Technology assessment
Velocity measurement
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Study of high speed combustion flows by laser velocimetry
Record Nr. UNINA-9910700813203321
Schaefer H. J  
Saint-Louis, France : , : [Insitut Franco-Allemand de Recherches]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena / / Michael A. Kegerise and Dan H. Neuhart
Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena / / Michael A. Kegerise and Dan H. Neuhart
Autore Kegerise Michael A.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2016
Descrizione fisica 1 online resource (118 pages) : color illustrations
Collana NASA/TM
Soggetto topico Body-wing configurations
Flow distribution
Laser doppler velocimeters
Reynolds number
Subsonic wind tunnels
Wind tunnel models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707928203321
Kegerise Michael A.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

Data di pubblicazione