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Record Nr. |
UNINA9910697186003321 |
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Autore |
DeSpirito James |
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Titolo |
Numerical investigation of aerodynamics of canard-controlled missile using planar and grid tail fins . Part II Subsonic and transonic flow [[electronic resource] /] / by James DeSpirito, Milton E. Vaughn, Jr., and W. David Washington |
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Pubbl/distr/stampa |
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Aberdeen Proving Ground, MD : , : Army Research Laboratory, , [2004] |
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Descrizione fisica |
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1 online resource (x, 92 pages) : color illustrations |
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Collana |
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Altri autori (Persone) |
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VaughnMilton E |
WashingtonW. David |
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Soggetti |
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Rockets (Aeronautics) - Canard fins - Aerodynamics - Models |
Rockets (Aeronautics) - Fins - Aerodynamics - Models |
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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 on Apr. 1, 2011). |
"March 2004." |
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