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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)  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2014
Materiale a stampa
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)  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2001
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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)  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2005]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1998
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , September 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Division, , November 1987
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 2020
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

Data di pubblicazione