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Record Nr. |
UNINA9910702683003321 |
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Autore |
Penland Jim A. |
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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 |
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Pubbl/distr/stampa |
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Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1979 |
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Descrizione fisica |
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1 online resource (144 pages) : illustrations |
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Collana |
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NASA technical paper ; ; 1552 |
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Soggetti |
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Aerodynamics |
Aerodynamic characteristics |
Computational fluid dynamics |
Delta wings |
Hypersonic aircraft |
Wind tunnel tests |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Title from title screen (viewed Sept. 22, 2014). |
"December 1979." |
"Performing organization, NASA Langley Research Center"--Technical report documentation page. |
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Nota di bibliografia |
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Includes bibliographical references (pages 20-22). |
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