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Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 / / Francis J. Capone, E. Ann Bare, Dorothy Arbiter
| Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 / / Francis J. Capone, E. Ann Bare, Dorothy Arbiter |
| Autore | Capone Francis J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (102 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Fighter aircraft
Aerodynamic characteristics Aerodynamic configurations Supersonic aircraft Computer programs Supersonic fighter planes Aerodynamics, Supersonic |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709714203321 |
Capone Francis J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Assessment of NASA's aircraft noise prediction capability [[electronic resource] /] / Milo D. Dahl, editor
| Assessment of NASA's aircraft noise prediction capability [[electronic resource] /] / Milo D. Dahl, editor |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (xxxi, 354 pages) : color illustrations |
| Altri autori (Persone) | DahlMilo D. <1956-> |
| Collana | NASA/TP |
| Soggetto topico |
Aeroacoustics
Noise prediction (aircraft) Jet aircraft noise Wind tunnel tests Hypersonic aircraft Subsonic aircraft Rotary wing aircraft Computational fluid dynamics Aircraft noise Supersonic aircraft |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702210303321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel [[electronic resource] /] / Rodrick V. Chima and Stefanie M. Hirt, Robert Reger
| Axisymmetric calculations of a low-boom inlet in a supersonic wind tunnel [[electronic resource] /] / Rodrick V. Chima and Stefanie M. Hirt, Robert Reger |
| Autore | Chima Rodrick V |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (12 pages) : illustrations (chiefly color) |
| Altri autori (Persone) |
HirtStefanie M
RegerRobert |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic inlets
Computational fluid dynamics Mass flow Flight paths Supersonic aircraft Stability |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701560503321 |
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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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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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Data quality assurance for supersonic jet noise measurements [[electronic resource] /] / Clifford A. Brown, Brenda S. Henderson, and James E. Bridges ; prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010
| Data quality assurance for supersonic jet noise measurements [[electronic resource] /] / Clifford A. Brown, Brenda S. Henderson, and James E. Bridges ; prepared for the Turbo Expo 2010 sponsored by the American Society of Mechanical Engineers (ASME), Glasgow, Scotland, United Kingdom, June 14-18, 2010 |
| Autore | Brown Clifford A (Clifford Alan) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (13 pages) : illustrations (color) |
| Altri autori (Persone) |
HendersonBrenda S
BridgesJames E |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamic noise
Supersonic aircraft Noise reduction Noise measurement Jet aircraft noise Exhaust gases Aeroacoustics Noise intensity |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699909503321 |
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Brown Clifford A (Clifford Alan)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Enabling rapid and robust structural analysis during conceptual design / / Lloyd B. Eldred, Sharon L. Padula, and Wu Li
| Enabling rapid and robust structural analysis during conceptual design / / Lloyd B. Eldred, Sharon L. Padula, and Wu Li |
| Autore | Eldred Lloyd B. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 2015 |
| Descrizione fisica | 1 online resource (21 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Structural analysis
Aerodynamic loads Supersonic aircraft Body-wing configurations Design analysis |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703786703321 |
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Eldred Lloyd B.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , February 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Exhaust nozzle plume effects on sonic boom test results for isolated nozzles [[electronic resource] /] / Raymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20
| Exhaust nozzle plume effects on sonic boom test results for isolated nozzles [[electronic resource] /] / Raymond S. Castner ; prepared for the 28th Applied Aerodynamics Conference sponsored by the American Institute of Aeronautics and Astronautics, Chicago, Illinois, June 28-July 1, 20 |
| Autore | Castner Raymond S |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011] |
| Descrizione fisica | 1 online resource (16 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Exhaust nozzles
Nozzle flow Plumes Supersonic aircraft Computational fluid dynamics Nozzle geometry Pressure ratio Shock waves Elastic waves |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701912103321 |
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Castner Raymond S
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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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Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [[electronic resource] /] / Raymond Castner
| Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [[electronic resource] /] / Raymond Castner |
| Autore | Castner Raymond S |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
| Descrizione fisica | 1 online resource (16 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Exhaust nozzles
Sonic booms Computational fluid dynamics Elastic waves Plumes F-15 aircraft Supersonic aircraft Pressure ratio |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701950003321 |
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Castner Raymond S
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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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Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models / / Susan E. Cliff [and four others]
| Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models / / Susan E. Cliff [and four others] |
| Autore | Cliff Susan E. |
| Pubbl/distr/stampa | Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , January 2015 |
| Descrizione fisica | 1 online resource (258 pages) : color illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Sonic booms
Supersonic aircraft Aircraft configurations Computational fluid dynamics Supersonic test apparatus |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703964503321 |
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Cliff Susan E.
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| Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , January 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / / Jimmy L. Pittman and Gregory D. Riebe
| Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 / / Jimmy L. Pittman and Gregory D. Riebe |
| Autore | Pittman Jimmy L. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 |
| Descrizione fisica | 1 online resource (113 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Aerodynamic characteristics
Aerodynamic configurations Angle of attack Hypersonic aircraft Supersonic aircraft |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707455703321 |
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Pittman Jimmy L.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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