| contributor author | P. N. Koch | |
| contributor author | A. Barlow | |
| contributor author | J. K. Allen | |
| contributor author | F. Mistree | |
| date accessioned | 2017-05-08T23:57:21Z | |
| date available | 2017-05-08T23:57:21Z | |
| date copyright | December, 1998 | |
| date issued | 1998 | |
| identifier issn | 1050-0472 | |
| identifier other | JMDEDB-27656#702_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/120855 | |
| description abstract | In this Technical Brief we illustrate the efficacy of the Robust Concept Exploration Method as applied to the preliminary design of a turbine lift engine for Advanced Short Take-Off and Vertical Landing (ASTOVL) fighter aircraft. This example is defined in collaboration with the Rolls-Royce Atlanta Engineering Group. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Facilitating Concept Exploration for Configuring Turbine Propulsion Systems | |
| type | Journal Paper | |
| journal volume | 120 | |
| journal issue | 4 | |
| journal title | Journal of Mechanical Design | |
| identifier doi | 10.1115/1.2829334 | |
| journal fristpage | 702 | |
| journal lastpage | 706 | |
| identifier eissn | 1528-9001 | |
| keywords | Propulsion systems | |
| keywords | Turbines | |
| keywords | Aircraft | |
| keywords | Collaboration | |
| keywords | Engines AND Design | |
| tree | Journal of Mechanical Design:;1998:;volume( 120 ):;issue: 004 | |
| contenttype | Fulltext | |
