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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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Transonic investigation of two-dimensional nozzles designed for supersonic cruise / / Francis J. Capone and Karen A. Deere
| Transonic investigation of two-dimensional nozzles designed for supersonic cruise / / Francis J. Capone and Karen A. Deere |
| Autore | Capone Francis J. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015 |
| Descrizione fisica | 1 online resource (iii, 311 pages) : color illustration |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Pressure drag Convergent-divergent nozzles Transonic nozzles Reynolds stress |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704024703321 |
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Capone Francis J.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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