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Record Nr. |
UNINA9910713894003321 |
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Autore |
Chapman Dean R. |
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Titolo |
Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range / / by Dean R. Chapman |
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Pubbl/distr/stampa |
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Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 |
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Descrizione fisica |
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1 online resource (44 pages) : illustrations |
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Collana |
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Technical notes / National Advisory Committee for Aeronautics ; ; No. 2787 |
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Soggetti |
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Aerodynamic load |
Aerodynamics, Supersonic |
Aerofoils |
Drag (Aerodynamics) |
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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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"September 17, 1952." |
No Federal Depository Library Program (FDLP) item number. |
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Nota di bibliografia |
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Includes bibliographical references (page 24). |
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