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The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals / / by Max M. Munk
| The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals / / by Max M. Munk |
| Autore | Munk Max M (Max Michael), <1890-> |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 |
| Descrizione fisica | 1 online resource (9 pages, 2 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Lift (Aerodynamics)
Angle of attack (Aerodynamics) Aerofoils Camber (Aerofoils) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713358403321 |
Munk Max M (Max Michael), <1890->
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| [Washington, D.C.] : , : National Advisory Committee for Aeronautics, , 1923 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers / / by Donald J. Graham
| The development of cambered airfoil sections having favorable lift characteristics at supercritical Mach numbers / / by Donald J. Graham |
| Autore | Graham Donald J. |
| Pubbl/distr/stampa | Washington : , : National Advisory Committee for Aeronautics, , December 1948 |
| Descrizione fisica | 1 online resource (82 pages) : illustrations |
| Collana | National Advisory Committee for Aeronautics technical note |
| Soggetto topico |
Airfoils
Aircraft stability Aircraft control Aerofoils Camber (Aerofoils) Lift (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717079703321 |
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Graham Donald J.
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| Washington : , : National Advisory Committee for Aeronautics, , December 1948 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 / / by Emma Jean Landrum and Barrett L. Shrout
| Effect of shape changes on the aerodynamic characteristics of a twisted and cambered arrow wing at Mach number 2.03 / / by Emma Jean Landrum and Barrett L. Shrout |
| Autore | Landrum Emma Jean |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Aerodynamics, Supersonic
Camber (Aerofoils) Mach number Reynolds number |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715060103321 |
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Landrum Emma Jean
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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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Effect of wing design on the longitudinal aerodynamic characteristics of a wing-body model at subsonic speeds / / by William P. Henderson and Jarrett K. Huffman
| Effect of wing design on the longitudinal aerodynamic characteristics of a wing-body model at subsonic speeds / / by William P. Henderson and Jarrett K. Huffman |
| Autore | Henderson William P. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1972 |
| Descrizione fisica | 1 online resource (58 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerodynamics
Subsonic speed Camber Airplanes - Wings - Design and construction Stability of airplanes, Longitudinal Camber (Aerofoils) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716529803321 |
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Henderson William P.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , December 1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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