Computational aerodynamic simulations of a 1215 ft/sec tip speed transonic fan system model for acoustic methods assessment and development / / Daniel L. Tweedt
| Computational aerodynamic simulations of a 1215 ft/sec tip speed transonic fan system model for acoustic methods assessment and development / / Daniel L. Tweedt |
| Autore | Tweedt Daniel L (Daniel Lawrence) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2014 |
| Descrizione fisica | 1 online resource (46 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Acoustic measurement
Flow distribution Boundary layers Nacelles Prediction analysis techniques Aerodynamic characteristics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703549703321 |
Tweedt Daniel L (Daniel Lawrence)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2014 | ||
| Lo trovi qui: Univ. Federico II | ||
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Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development / / Daniel L. Tweedt
| Computational aerodynamic simulations of an 840 ft/sec tip speed advanced ducted propulsor fan system model for acoustic methods assessment and development / / Daniel L. Tweedt |
| Autore | Tweedt Daniel L (Daniel Lawrence) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2014 |
| Descrizione fisica | 1 online resource (52 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Computational fluid dynamics
Ducted fans Acoustic measurement Flow distribution Prediction analysis techniques Nacelles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703549603321 |
Tweedt Daniel L (Daniel Lawrence)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2014 | ||
| Lo trovi qui: Univ. Federico II | ||
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Design and integration of a rotor alone nacelle for acoustic fan testing / / Tony D. Shook [and five others]
| Design and integration of a rotor alone nacelle for acoustic fan testing / / Tony D. Shook [and five others] |
| Autore | Shook Tony D. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2001 |
| Descrizione fisica | 1 online resource (8 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Rotor blades (turbomachinery)
Rotors Fan blades Turbomachine blades Nacelles Aerodynamic configurations Design analysis |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706550103321 |
Shook Tony D.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2001 | ||
| Lo trovi qui: Univ. Federico II | ||
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Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration / / Lawrence E. Putnam
| Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration / / Lawrence E. Putnam |
| Autore | Putnam Lawrence E (Lawrence Elwood) |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (67 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Aerodynamic characteristics
Transonic speed Wind tunnel tests Nacelles Transport aircraft Airplanes - Nacelles Transport planes - Design and construction Stability of airplanes, Longitudinal |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709713903321 |
Putnam Lawrence E (Lawrence Elwood)
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 | ||
| Lo trovi qui: Univ. Federico II | ||
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An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts [[electronic resource] /] / Robert J. Mack
| An evaluation of measured pressure signatures from wind-tunnel models of three low-boom concepts [[electronic resource] /] / Robert J. Mack |
| Autore | Mack Robert J |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2005] |
| Descrizione fisica | 1 online resource (24 pages) : illustrations |
| Collana | NASA/TM- |
| Soggetto topico |
Sonic booms
Flow distribution Design analysis Nacelles Interference lift Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697004603321 |
Mack Robert J
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2005] | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental and theoretical study of flow fields around ducted-nacelle models / / Robert J. Mack
| Experimental and theoretical study of flow fields around ducted-nacelle models / / Robert J. Mack |
| Autore | Mack Robert J. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1998 |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Nacelles
Ducted flow Mach number Ducted bodies Flow characteristics Fluid flow Angle of attack Aircraft design |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705868803321 |
Mack Robert J.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1998 | ||
| 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 |
Baumeister Kenneth J.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , September 1996 | ||
| Lo trovi qui: Univ. Federico II | ||
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Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport / / Milton Lamb, John R. Carlson, and Odis C. Pendergraft
| Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport / / Milton Lamb, John R. Carlson, and Odis C. Pendergraft |
| Autore | Lamb Milton |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , November 1987 |
| Descrizione fisica | 1 online resource (21 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Angle of attack
Nacelles Separated flow Supersonic flow Transonic wind tunnels |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707804103321 |
Lamb Milton
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , November 1987 | ||
| Lo trovi qui: Univ. Federico II | ||
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Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds / / Robert J. Mack
| Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds / / Robert J. Mack |
| Autore | Mack Robert J. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999 |
| Descrizione fisica | 1 online resource (15 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamic characteristics
Body-wing configurations Nacelles Sonic booms Wings Aerodynamic configurations Supersonic flight Aerodynamic noise Noise reduction Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706143703321 |
Mack Robert J.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999 | ||
| Lo trovi qui: Univ. Federico II | ||
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An over-the-rotor liner investigation with configurations enabled by additive manufacturing / / Michael G. Jones
| An over-the-rotor liner investigation with configurations enabled by additive manufacturing / / Michael G. Jones |
| Autore | Jones Michael G. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 2020 |
| Descrizione fisica | 1 online resource (17 pages, 1 unnumbered page) : illustrations (mostly color) |
| Collana | NASA/TM |
| Soggetto topico |
Acoustics
Configurations Nacelles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715364203321 |
Jones Michael G.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 2020 | ||
| Lo trovi qui: Univ. Federico II | ||
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