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Autore: | Penland Jim A. |
Titolo: | Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 / / Jim A. Penland, James B. Hallissy, and James L. Dillon |
Pubblicazione: | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1979 |
Descrizione fisica: | 1 online resource (144 pages) : illustrations |
Soggetto topico: | Aerodynamics |
Aerodynamic characteristics | |
Computational fluid dynamics | |
Delta wings | |
Hypersonic aircraft | |
Wind tunnel tests | |
Persona (resp. second.): | HallissyJames B. |
DillonJames L. | |
Note generali: | Title from title screen (viewed Sept. 22, 2014). |
"December 1979." | |
"Performing organization, NASA Langley Research Center"--Technical report documentation page. | |
Nota di bibliografia: | Includes bibliographical references (pages 20-22). |
Titolo autorizzato: | Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 |
Formato: | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione: | Inglese |
Record Nr.: | 9910702683003321 |
Lo trovi qui: | Univ. Federico II |
Opac: | Controlla la disponibilitĂ qui |