| contributor author | Kaul, Upender K. | |
| contributor author | Nguyen, Nhan T. | |
| date accessioned | 2019-02-28T10:59:37Z | |
| date available | 2019-02-28T10:59:37Z | |
| date copyright | 5/18/2018 12:00:00 AM | |
| date issued | 2018 | |
| identifier issn | 0098-2202 | |
| identifier other | fe_140_10_101108.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4251517 | |
| description abstract | A Reynolds-averaged Navier–Stokes (RANS) computational study was conducted to investigate the effect of various variable camber continuous trailing edge flap (VCCTEF) configurations on the lift and drag of a NASA generic transport model (GTM) wing section. Out of the five two-dimensional (2D) VCCTEF configurations considered with varying camber in the three-segment flap region, with a total deflection of 6 deg, the best stall performance was exhibited by the circular and parabolic arc camber flaps. Both circular and parabolic arc flaps give similar lift performance, with the circular arc yielding a higher lift coefficient and parabolic arc resulting in the lowest drag and hence the best L/D performance at design Cl. Analysis of results based on linear theory shows excellent agreement between computed and theoretical incremental lift. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Drag Characterization Study of Variable Camber Continuous Trailing Edge Flap | |
| type | Journal Paper | |
| journal volume | 140 | |
| journal issue | 10 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.4040070 | |
| journal fristpage | 101108 | |
| journal lastpage | 101108-13 | |
| tree | Journal of Fluids Engineering:;2018:;volume( 140 ):;issue: 010 | |
| contenttype | Fulltext | |
