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.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012 | ||
| 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.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2013 | ||
| 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.
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| Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , February 2016 | ||
| Lo trovi qui: Univ. Federico II | ||
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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.
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| Cincinnati, Ohio : , : General Electric Company, Aircraft Engine Business Group, , February, 1984 | ||
| Lo trovi qui: Univ. Federico II | ||
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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.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Lo trovi qui: Univ. Federico II | ||
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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
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Lo trovi qui: Univ. Federico II | ||
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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
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1996 | ||
| Lo trovi qui: Univ. Federico II | ||
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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
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| Saint-Louis, France : , : [Insitut Franco-Allemand de Recherches] | ||
| Lo trovi qui: Univ. Federico II | ||
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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.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2016 | ||
| Lo trovi qui: Univ. Federico II | ||
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