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Acoustic calibration apparatus for calibrating plethysmographic acoustic pressure sensors [[electronic resource] /] / inventors, Allan J. Zuckerwar, David C. Davis
| Acoustic calibration apparatus for calibrating plethysmographic acoustic pressure sensors [[electronic resource] /] / inventors, Allan J. Zuckerwar, David C. Davis |
| Edizione | [[Redacted ed.]] |
| Pubbl/distr/stampa | [Washington, DC] : , : [National Aeronautics and Space Administration], , [1994] |
| Descrizione fisica | 1 online resource : illustrations |
| Altri autori (Persone) |
ZuckerwarAllan J
DavisDavid C. L |
| Collana | NASA case |
| Soggetto topico |
Acoustic impedance
Acoustic measurement Plethysmography Pressure measurement Pressure sensors |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697270103321 |
| [Washington, DC] : , : [National Aeronautics and Space Administration], , [1994] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Active combustion control for aircraft gas-turbine engines [[electronic resource] ] : experimental results for an advanced, low-emissions combustor prototype / / John C. DeLaat ... [and others]
| Active combustion control for aircraft gas-turbine engines [[electronic resource] ] : experimental results for an advanced, low-emissions combustor prototype / / John C. DeLaat ... [and others] |
| Autore | DeLaat John C. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (19 pages) : illustrations (some color) |
| Altri autori (Persone) | DeLaatJohn C |
| Collana | NASA/TM |
| Soggetto topico |
Combustion stability
Gas turbine engines Pressure sensors Combustion chambers Dynamic pressure Adaptive control Combustion control |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Active combustion control for aircraft gas-turbine engines |
| Record Nr. | UNINA-9910702217703321 |
DeLaat John C.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| 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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Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight [[electronic resource] ] : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / / Anthony Neal Watkins ... [and others]
| Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight [[electronic resource] ] : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / / Anthony Neal Watkins ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (18 pages) : color illustrations |
| Altri autori (Persone) | WatkinsAnthony Neal |
| Collana | NASA/TM |
| Soggetto topico |
Pressure measurement
Pressure sensitive paints Flow distribution Flight simulation Pressure sensors Horizontal flight Blade tips |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight |
| Record Nr. | UNINA-9910701779103321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Design and evaluation of a new boundary layer rake for flight testing / / Trong T. Bui and David L. Oates, Jose c. Gonsalez
| Design and evaluation of a new boundary layer rake for flight testing / / Trong T. Bui and David L. Oates, Jose c. Gonsalez |
| Autore | Bui Trong T. |
| Pubbl/distr/stampa | Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , January 2000 |
| Descrizione fisica | 1 online resource (16 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Boundary layers
Pressure sensors Design analysis Structural design Flight test instruments |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706265103321 |
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Bui Trong T.
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| Edwards, California : , : National Aeronautics and Space Administration, Dryden Flight Reserch Center, , January 2000 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Development of optical diaphragm deflection sensors [[electronic resource] ] : final report / / W.L. Ghering ... [and others]
| Development of optical diaphragm deflection sensors [[electronic resource] ] : final report / / W.L. Ghering ... [and others] |
| Pubbl/distr/stampa | [Alliance, Ohio] : , : The Babcock & Wilcox Company, Research and Development Division ; Cleveland, Ohio : , : National Aeronautics and Space Administration, NASA Lewis Research Center, , [1985?] |
| Descrizione fisica | 1 online resource (vi, 48 pages) : illustrations |
| Altri autori (Persone) | GheringW. L |
| Collana | [NASA contractor report] |
| Soggetto topico |
Aircraft engines
Diaphragms (mechanics) Fiber optics Hermetic seals High temperature Optical measuring instruments Overpressure Pressure measurement Pressure sensors Room temperature Silicon |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Development of optical diaphragm deflection sensors |
| Record Nr. | UNINA-9910701722503321 |
| [Alliance, Ohio] : , : The Babcock & Wilcox Company, Research and Development Division ; Cleveland, Ohio : , : National Aeronautics and Space Administration, NASA Lewis Research Center, , [1985?] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Evaluation of data-logging transducer to passively collect pressure vessel p/T history / / Stephen P. Wnuk, Son Le, Raymond A. Loew
| Evaluation of data-logging transducer to passively collect pressure vessel p/T history / / Stephen P. Wnuk, Son Le, Raymond A. Loew |
| Autore | Wnuk Stephen P. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 |
| Descrizione fisica | 1 online resource (7 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Pressure vessels
Pressure sensors Fatigue life Failure analysis Pressure recorders |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704876003321 |
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Wnuk Stephen P.
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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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An experimental evaluation of the performance of two combination pitot pressure probes [[electronic resource] /] / David J. Arend and John D. Saunders ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
| An experimental evaluation of the performance of two combination pitot pressure probes [[electronic resource] /] / David J. Arend and John D. Saunders ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009 |
| Autore | Arend David J |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] |
| Descrizione fisica | 1 online resource (17 pages) : illustrations |
| Altri autori (Persone) | SaundersJohn D |
| Collana | NASA TM- |
| Soggetto topico |
Mach number
Pitch (inclination) Pressure sensors Aerodynamics Pitot tubes Pressure measurement Pneumatic probes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910696931403321 |
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Arend David J
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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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 |
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Grosser Wendy I.
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| 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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Flight test results from the rake airflow gage experiment on the F-15B airplane [[electronic resource] /] / Michael A. Frederick and Nalin A. Ratnayake
| Flight test results from the rake airflow gage experiment on the F-15B airplane [[electronic resource] /] / Michael A. Frederick and Nalin A. Ratnayake |
| Autore | Frederick Michael A |
| Pubbl/distr/stampa | Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2011] |
| Descrizione fisica | 1 online resource (28 pages) : illustrations (some color) |
| Altri autori (Persone) | RatnayakeNalin A |
| Collana | NASA/TM |
| Soggetto topico |
Air flow
Dynamic pressure Flight tests Flow distribution Flow deflection Pressure sensors |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702299703321 |
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Frederick Michael A
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| Edwards, CA : , : National Aeronautics and Space Administration, Dryden Flight Research Center, , [2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
-
Pressure sensors
(18)
- Pressure measurement (5)
- Flight tests (3)
- Wind tunnel tests (3)
- Dynamic pressure (2)