Loading...
Please wait, while we are loading the content...
Similar Documents
Experimental result analysis for scaled model of UiTM tailless blended wing-body (BWB) Baseline 7 unmanned aerial vehicle (UAV)
| Content Provider | Scilit |
|---|---|
| Author | Nasir, R. E. M. Ahmad, A. M. Latif, Z. A. A. Saad, R. M. Kuntjoro, W. |
| Copyright Year | 2017 |
| Description | Journal: Iop Conference Series: Materials Science and Engineering Blended wing-body (BWB) aircraft having planform configuration similar to those previously researched and published by other researchers does not guarantee that an efficient aerodynamics in term of lift-to-drag ratio can be achieved. In this wind tunnel experimental study, BWB half model is used. The model is also being scaled down to 71.5% from the actual size. Based on the results, the maximum lift coefficient is found to be 0.763 when the angle is at 27.5° after which the model starts to stall. The minimum drag coefficient is 0.014, measured at zero angle of attack. The corrected lift-to-drag ratio (L/D) is 15.9 at angle 7.8°. The scaled model has a big flat surface that surely gives an inaccurate data but the data obtained shall give some insights for future perspective towards the BWB model being tested. |
| Related Links | http://iopscience.iop.org/article/10.1088/1757-899X/270/1/012005/pdf |
| ISSN | 17578981 |
| e-ISSN | 1757899X |
| DOI | 10.1088/1757-899x/270/1/012005 |
| Journal | Iop Conference Series: Materials Science and Engineering |
| Issue Number | 1 |
| Volume Number | 270 |
| Language | English |
| Publisher | IOP Publishing |
| Publisher Date | 2017-12-01 |
| Access Restriction | Open |
| Subject Keyword | Journal: Iop Conference Series: Materials Science and Engineering |
| Content Type | Text |
| Resource Type | Article |
