| |
|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910703769103321 |
|
|
Autore |
Herrick Gregory Paul <1972-> |
|
|
Titolo |
Assessing fan flutter stability in presence of inlet distortion using one-way and two-way coupled methods / / Gregory P. Herrick |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2014 |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (17 pages) : color illustrations |
|
|
|
|
|
|
Collana |
|
|
|
|
|
|
Soggetti |
|
Turbomachinery |
Flutter analysis |
Inlet flow |
Computational fluid dynamics |
Aeroelasticity |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
Title from title screen (viewed on June 3, 2015). |
"December 2014." |
"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014." |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (pages 15-17). |
|
|
|
|
|
| |