Info
- Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.
Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range / / by Dean R. Chapman
| Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range / / by Dean R. Chapman |
| Autore | Chapman Dean R. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 |
| Descrizione fisica | 1 online resource (44 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamic load
Aerodynamics, Supersonic Aerofoils Drag (Aerodynamics) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713894003321 |
Chapman Dean R.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
An analysis of base pressure at supersonic velocities and comparison with experiment / / by Dean R. Chapman
| An analysis of base pressure at supersonic velocities and comparison with experiment / / by Dean R. Chapman |
| Autore | Chapman Dean R. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1950 |
| Descrizione fisica | 1 online resource (69 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamics, Supersonic
Aerofoils Axial flow Inviscid flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713756703321 |
|
Chapman Dean R.
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1950 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||