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Acoustic mode measurements in the inlet of a model turbofan using a continuously rotating rake [[electronic resource] /] / Laurence J. Heidelberg and David G. Hall
| Acoustic mode measurements in the inlet of a model turbofan using a continuously rotating rake [[electronic resource] /] / Laurence J. Heidelberg and David G. Hall |
| Autore | Heidelberg Laurence J |
| Pubbl/distr/stampa | [Washington, DC] : , : [National Aeronautics and Space Administration], , [1992] |
| Descrizione fisica | 1 online resource (30 pages) : digital, PDF file |
| Altri autori (Persone) | HallDavid G (Engineer) |
| Collana | NASA technical memorandum |
| Soggetto topico |
Acoustic measurement
Acoustic properties Ducted fan engines Engine inlets Engine noise Jet aircraft noise Microphones Propagation models Shrouded propellers |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699534203321 |
Heidelberg Laurence J
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| [Washington, DC] : , : [National Aeronautics and Space Administration], , [1992] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model / / Jeffrey T. Csank and Thomas J. Stueber
| Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model / / Jeffrey T. Csank and Thomas J. Stueber |
| Autore | Csank Jeffrey T. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2013] |
| Descrizione fisica | 1 online resource (12 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Inlet flow
Controllers Feedback control Computerized simulation Turbine engines Engine inlets |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704816803321 |
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Csank Jeffrey T.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2013] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet / / Colin S. Bidwell
| Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet / / Colin S. Bidwell |
| Autore | Bidwell Colin S. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National National Aeronautics and Space Administration, Lewis Research Center, , February 1997 |
| Descrizione fisica | 1 online resource (26 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Boeing 737 aircraft
Ice formation Prediction analysis techniques Engine inlets Inlet pressure |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707328303321 |
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Bidwell Colin S.
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| Cleveland, Ohio : , : National National Aeronautics and Space Administration, Lewis Research Center, , February 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design / / Randy Thomas and Thomas J. Stueber
| Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design / / Randy Thomas and Thomas J. Stueber |
| Autore | Thomas Randy |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013 |
| Descrizione fisica | 1 online resource (24 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Actuators
Control equipment Data acquisition Engine inlets Feedback control Hardware-in-the-loop simulation Pressure sensors Supersonic wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Combined cycle engine large-scale inlet for mode transition experiments |
| Record Nr. | UNINA-9910705296403321 |
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Thomas Randy
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Computational analysis of a low-boom supersonic inlet [[electronic resource] /] / Rodrick V. Chima
| Computational analysis of a low-boom supersonic inlet [[electronic resource] /] / Rodrick V. Chima |
| Autore | Chima Rodrick V |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (14 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Engine inlets Supersonic aircraft Supersonic inlets Inlet airframe configurations Overpressure Supersonic flow Sonic booms Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701537703321 |
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Chima Rodrick V
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Determination of shed ice particle size using high speed digital imaging / / Howard Broughton [and three others]
| Determination of shed ice particle size using high speed digital imaging / / Howard Broughton [and three others] |
| Autore | Broughton Howard |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , February 1997 |
| Descrizione fisica | 1 online resource (8 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aircraft icing
Engine inlets Ice formation Image analysis Imaging techniques |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707837703321 |
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Broughton Howard
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , February 1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section [[electronic resource] /] / Robert Tornabene
| Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section [[electronic resource] /] / Robert Tornabene |
| Autore | Tornabene Robert |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005] |
| Descrizione fisica | 1 online resource (15 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Air flow
Characterization Engine inlets Pulse detonation engines Supersonic wind tunnels Gas valves Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697023103321 |
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Tornabene Robert
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2005] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Dynamic testing of the NASA Hypersonic Project combined cycle engine testbed for mode transition experiments [[electronic resource] /] / T.J. Stueber ... [and others]
| Dynamic testing of the NASA Hypersonic Project combined cycle engine testbed for mode transition experiments [[electronic resource] /] / T.J. Stueber ... [and others] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (25 pages) : color illustrations |
| Altri autori (Persone) | StueberT. J |
| Collana | NASA/TM |
| Soggetto topico |
Air flow
Engine inlets Dynamic tests Hypersonic speed Propulsion system configurations Turbine engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Dynamic testing of the National Aeronautics and Space Administration Hypersonic Project combined cycle engine testbed for mode transition experiments |
| Record Nr. | UNINA-9910701542903321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet / / Michael Papadakis [and six others]
| Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet / / Michael Papadakis [and six others] |
| Autore | Papadakis Michael |
| Pubbl/distr/stampa | Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 |
| Descrizione fisica | 1 online resource (430 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Water
Drops (liquids) Impingement Airfoils Wings Engine inlets |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705699503321 |
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Papadakis Michael
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| Cleveland Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design / / Kenneth J. Baumeister and Kevin L. Kreider
| Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design / / Kenneth J. Baumeister and Kevin L. Kreider |
| Autore | Baumeister Kenneth J. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , September 1996 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Finite difference theory
Time marching Nacelles Sound propagation Aircraft engines Engine inlets |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Finite difference time marching in the frequency domain |
| Record Nr. | UNINA-9910707250903321 |
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Baumeister Kenneth J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , September 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Engine inlets
(24)
- Turbine engines (5)
- Wind tunnel tests (5)
- Computational fluid dynamics (4)
- Air flow (3)