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Effect of retractable-spoiler location on rolling- and yawing-moment coefficents / / J.A. Shortal
| Effect of retractable-spoiler location on rolling- and yawing-moment coefficents / / J.A. Shortal |
| Autore | Shortal Joseph Adams <1908-> |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 |
| Descrizione fisica | 1 online resource (12 pages, 5 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Spoilers (Airplanes)
Flaps (Airplanes) Airplanes - Control surfaces Rolling (Aerodynamics) Yawing (Aerodynamics) Wind tunnel testing |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716911103321 |
Shortal Joseph Adams <1908->
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Preliminary stability and control tests in the NACA free-flight wind tunnel and correlation with full-scale flight tests / / by Joseph A. Shortal and Clatyon J. Osterhout
| Preliminary stability and control tests in the NACA free-flight wind tunnel and correlation with full-scale flight tests / / by Joseph A. Shortal and Clatyon J. Osterhout |
| Autore | Shortal Joseph Adams <1908-> |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 |
| Descrizione fisica | 1 online resource (19 pages, 10 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Control
Stability of airplanes Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717251403321 |
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Shortal Joseph Adams <1908->
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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