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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| Autore: |
Chapman Dean R.
|
| Titolo: |
Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range / / by Dean R. Chapman
|
| Pubblicazione: | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 |
| Descrizione fisica: | 1 online resource (44 pages) : illustrations |
| Soggetto topico: | Aerodynamic load |
| Aerodynamics, Supersonic | |
| Aerofoils | |
| Drag (Aerodynamics) | |
| Note generali: | "September 17, 1952." |
| No Federal Depository Library Program (FDLP) item number. | |
| Nota di bibliografia: | Includes bibliographical references (page 24). |
| Titolo autorizzato: | Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910713894003321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |