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Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 / / by Odell A. Morris and Robert J. Mack
| Aerodynamic characteristics of a parasol-wing--body combination utilizing favorable lift interference at Mach numbers from 3.00 to 4.63 / / by Odell A. Morris and Robert J. Mack |
| Autore | Morris Odell A. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 |
| Descrizione fisica | 1 online resource (36 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Airplanes - Wings
Lift (Aerodynamics) Interference (Aerodynamics) Aerodynamics |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714075203321 |
Morris Odell A.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds / / Harry W. Carlson and Robert J. Mack
| Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds / / Harry W. Carlson and Robert J. Mack |
| Autore | Carlson Harry W. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , November 1980 |
| Descrizione fisica | 1 online resource (81 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Aerodynamic characteristics
Computer programs Leading edge thrust Nonlinearity Supersonic speed Aerodynamics, Supersonic Airplanes - Wings Supersonic planes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707472303321 |
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Carlson Harry W.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , November 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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