Info
- Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.
Axial and centrifugal compressor mean line flow analysis method [[electronic resource] /] / Joseph P. Veres ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
| Axial and centrifugal compressor mean line flow analysis method [[electronic resource] /] / Joseph P. Veres ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009 |
| Autore | Veres Joseph P |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] |
| Descrizione fisica | 1 online resource (32 pages) : illustrations |
| Collana | NASA TM- |
| Soggetto topico |
Turbocompressors
Fluid flow Computational fluid dynamics Compressible fluids Design analysis Guide vanes Centrifugal compressors |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910696924603321 |
Veres Joseph P
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Compressor study to meet large civil tilt rotor engine requirements [[electronic resource] /] / Joseph P. Veres ; prepared for the 65th Annual Forum and Technology Display sponsored by the American Helicopter Society, Grapevine, Texas, May 27-29, 2009
| Compressor study to meet large civil tilt rotor engine requirements [[electronic resource] /] / Joseph P. Veres ; prepared for the 65th Annual Forum and Technology Display sponsored by the American Helicopter Society, Grapevine, Texas, May 27-29, 2009 |
| Autore | Veres Joseph P |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] |
| Descrizione fisica | 1 online resource (35 pages) : illustrations |
| Altri autori (Persone) | HenriksenStephen |
| Collana | NASA TM |
| Soggetto topico |
Compressors
Turbocompressors Tilt rotor aircraft Leading edges Rotary wing aircraft Engine design Flow velocity Centrifugal force Trailing edges |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697087203321 |
|
Veres Joseph P
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Dimension determination of precursive stall events in a single stage high speed compressor / / Michelle M. Bright, Helen K. Qammar and Tom T. Hartley
| Dimension determination of precursive stall events in a single stage high speed compressor / / Michelle M. Bright, Helen K. Qammar and Tom T. Hartley |
| Autore | Bright Michelle M. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1996 |
| Descrizione fisica | 1 online resource (10 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Turbocompressors
Rotating stalls Pressure measurement Chaos Power spectra |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707356203321 |
|
Bright Michelle M.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , July 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
An experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor / / Reid A. Berdanier and Nicole L. Key
| An experimental investigation of the flow physics associated with end wall losses and large rotor tip clearances as found in the rear stages of a high pressure compressor / / Reid A. Berdanier and Nicole L. Key |
| Autore | Berdanier Reid A. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015 |
| Descrizione fisica | 1 online resource (xiv, 145 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Wall flow
Turbocompressors Flow visualization Leakage Turbomachinery |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704241203321 |
|
Berdanier Reid A.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , September 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Final report for the advanced turbocharger design study program [[electronic resource] /] / by D. G. Culy and R. W. Heldenbrand and N. R. Richardson
| Final report for the advanced turbocharger design study program [[electronic resource] /] / by D. G. Culy and R. W. Heldenbrand and N. R. Richardson |
| Autore | Culy D. G |
| Pubbl/distr/stampa | [Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1984] |
| Descrizione fisica | 1 online resource (xiii, 184 pages) : digital, PDF file |
| Altri autori (Persone) |
HeldenbrandR. W
RichardsonN. R |
| Collana | NASA CR |
| Soggetto topico |
Engine design
Superchargers Technology transfer Turbocompressors Vibration effects |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Advanced turbocharger design study program |
| Record Nr. | UNINA-9910699741603321 |
|
Culy D. G
|
||
| [Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1984] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Integrated turbine tip clearance and gas turbine engine simulation / / Jeffryes W. Chapman [and three others]
| Integrated turbine tip clearance and gas turbine engine simulation / / Jeffryes W. Chapman [and three others] |
| Autore | Chapman Jeffryes W. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2016 |
| Descrizione fisica | 1 online resource (17 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Blade tips
Gas turbine engines Thermodynamics Turbine blades Turbocompressors |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707929203321 |
|
Chapman Jeffryes W.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Methods for computationally efficient structured CFD simulations of complex turbomachinery flows [[electronic resource] /] / Gregory P. Herrick, Jen-Ping Chen
| Methods for computationally efficient structured CFD simulations of complex turbomachinery flows [[electronic resource] /] / Gregory P. Herrick, Jen-Ping Chen |
| Autore | Herrick Gregory Paul <1972-> |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (13 pages) : color illustrations |
| Altri autori (Persone) | ChenJen-Ping |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Clearances Rotating stalls Time measurement Turbocompressors Turbomachinery |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702007103321 |
|
Herrick Gregory Paul <1972->
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Orifice mass flow calculation in NASA's W-8 single stage axial compressor facility / / Richard F. Bozak
| Orifice mass flow calculation in NASA's W-8 single stage axial compressor facility / / Richard F. Bozak |
| Autore | Bozak Richard F. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2018 |
| Descrizione fisica | 1 online resource (28 pages) : illustrations (mostly color) |
| Collana | NASA/TM |
| Soggetto topico |
Mass flow
Orifice flow Turbocompressors Discharge coefficient Static pressure |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Orifice mass flow calculation in NASA's W 8 single stage axial compressor facility |
| Record Nr. | UNINA-9910706861803321 |
|
Bozak Richard F.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project / / Joseph P. Veres
| Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project / / Joseph P. Veres |
| Autore | Veres Joseph P. |
| Pubbl/distr/stampa | Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2002 |
| Descrizione fisica | 1 online resource (5 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Gas turbine engines
Computational fluid dynamics Turbocompressors Turbines Combustion chambers |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Overview of high-fidelity modeling activities in the numerical propulsion system simulations |
| Record Nr. | UNINA-9910705401903321 |
|
Veres Joseph P.
|
||
| Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Performance estimates for the space station power system Brayton Cycle compressor and turbine / / Robert L. Cummings
| Performance estimates for the space station power system Brayton Cycle compressor and turbine / / Robert L. Cummings |
| Autore | Cummings Robert L. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , 1989 |
| Descrizione fisica | 1 online resource (31 pages) : illustrations |
| Collana | NASA contractor report |
| Soggetto topico |
Brayton cycle
Compressors Estimates Solar dynamic power systems Space Station Freedom Space station power supplies Turbocompressors |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705376103321 |
|
Cummings Robert L.
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , 1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Soggetto topico
-
Turbocompressors
(12)
- Computational fluid dynamics (4)
- Turbomachinery (3)
- Compressors (2)
- Engine design (2)