| |
|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910702216503321 |
|
|
Autore |
Shyam Vikram |
|
|
Titolo |
Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating [[electronic resource] /] / Vikram Shyam, Ali Ameri |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012] |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (8 pages) : illustrations (some color) |
|
|
|
|
|
|
Collana |
|
|
|
|
|
|
Altri autori (Persone) |
|
|
|
|
|
|
Soggetti |
|
Computational fluid dynamics |
Supersonic turbines |
Blade tips |
Supersonic flow |
Rotor aerodynamics |
Axial flow turbines |
Supersonic heat transfer |
Contours |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
Title from title screen (viewed on Dec. 3, 2012). |
"July 2012." |
"Prepared for the TURBO EXPO 2011 sponsored by the American Society of Mechanical Engineers (ASME) Vancouver, British Columbia, June 6-10, 2011." |
"GT2011-46390." |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (page 8). |
|
|
|
|
|
| |