Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow / / by M.J. Queijo
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| Autore: |
Queijo M. J.
|
| Titolo: |
Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow / / by M.J. Queijo
|
| Pubblicazione: | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968 |
| Descrizione fisica: | 1 online resource (76 pages) : illustrations |
| Soggetto topico: | Compressible flow |
| Stability derivatives | |
| Airplanes - Wings - Aerodynamics | |
| Rolling (Aerodynamics) | |
| Yawing (Aerodynamics) | |
| Note generali: | "December 1968." |
| Nota di bibliografia: | Includes bibliographical references (pages 40-41). |
| Titolo autorizzato: | Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910715901503321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |