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
(Visualizza in formato marc)
(Visualizza in BIBFRAME)
| 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 |