| dc.contributor.author | J. J. Adamczyk | |
| dc.contributor.author | R. A. Mulac | |
| dc.contributor.author | M. L. Celestina | |
| dc.date.accessioned | 2017-05-08T23:23:39Z | |
| dc.date.available | 2017-05-08T23:23:39Z | |
| dc.date.copyright | October, 1986 | |
| dc.date.issued | 1986 | |
| dc.identifier.issn | 0889-504X | |
| dc.identifier.other | JOTUEI-28578#180_1.pdf | |
| dc.identifier.uri | http://yetl.yabesh.ir/yetl/handle/yetl/101825 | |
| dc.description.abstract | A mathematical model is proposed for closing or mathematically completing the system of equations which describes the time-averaged flow field through the blade passages of multistage turbomachinery. These equations, referred to as the average-passage equation system, govern a conceptual model which has proven useful in turbomachinery aerodynamic design and analysis. The closure model is developed so as to insure a consistency between these equations and the axisymmetric through-flow equations. The closure model was incorporated into a computer code for use in simulating the flow field about a high-speed counterrotating propeller and a high-speed fan stage. Results from these simulations are presented. | |
| dc.publisher | The American Society of Mechanical Engineers (ASME) | |
| dc.title | A Model for Closing the Inviscid Form of the Average-Passage Equation System | |
| dc.type | Journal Paper | |
| dc.journal.volume | 108 | |
| dc.journal.issue | 2 | |
| dc.journal.title | Journal of Turbomachinery | |
| dc.identifier.doi | 10.1115/1.3262035 | |
| dc.journal.fristpage | 180 | |
| dc.journal.lastpage | 186 | |
| dc.identifier.eissn | 1528-8900 | |
| dc.tree | Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 002 | |
| dc.contenttype | Fulltext | |
