| contributor author | Louis B. Wonnell | |
| contributor author | Anthony Palazotto | |
| contributor author | Sivaguru Sritharan | |
| date accessioned | 2022-01-30T21:37:35Z | |
| date available | 2022-01-30T21:37:35Z | |
| date issued | 8/1/2020 12:00:00 AM | |
| identifier other | %28ASCE%29EM.1943-7889.0001810.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4268550 | |
| description abstract | The research reported herein makes use of finite-volume simulations of morphing continuum theory (MCT) to reproduce critical relations of thin-airfoil theory for the simple configuration of a flat plate for supersonic and subsonic flows. With a small mesh size of N=5,600 elements, simulations confirm that inviscid flows simulated by MCT match analytic relations for lift and pressure coefficients derived from classical fluid mechanics, a result confirmed by the inviscid MCT equations. Initial success of MCTHyperFOAM version 1.0 for the flat plate indicates that the solver can be extended to more complex aerodynamic flows. | |
| publisher | ASCE | |
| title | Incorporation of Morphing Theory to Aerodynamic Flows | |
| type | Journal Paper | |
| journal volume | 146 | |
| journal issue | 8 | |
| journal title | Journal of Engineering Mechanics | |
| identifier doi | 10.1061/(ASCE)EM.1943-7889.0001810 | |
| page | 11 | |
| tree | Journal of Engineering Mechanics:;2020:;Volume ( 146 ):;issue: 008 | |
| contenttype | Fulltext | |
