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.
Aeroservoelastic testing of free flying wind tunnel models / / Robert C. Scott [and four others]
| Aeroservoelastic testing of free flying wind tunnel models / / Robert C. Scott [and four others] |
| Autore | Scott Robert C. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 |
| Descrizione fisica | 1 online resource (2 volumes) : color illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Aeroservoelasticity
Flaps (control surfaces) Gust loads Semispan models Transonic wind tunnels Wind tunnel tests |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt 1. A sidewall supported semispan model tested for gust load alleviation and flutter suppression. -- pt 2. A centerline supported fullspan model tested for gust load alleviation. |
| Record Nr. | UNINA-9910702418703321 |
Scott Robert C.
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Subsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration / / Bryan A. Campbell [and seven others]
| Subsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration / / Bryan A. Campbell [and seven others] |
| Autore | Campbell Bryan A. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999 |
| Descrizione fisica | 1 online resource (128 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Boundary layer control
Leading edges Wind tunnel tests Flaps (control surfaces) Pressure effects Subsonic speed Supersonic transports Aerodynamic configurations |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Subsonic investigation of a leading-edge boundary layer control suction system on a high-speed civil transport configuration |
| Record Nr. | UNINA-9910706520903321 |
|
Campbell Bryan A.
|
||
| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
