Research Article
Influence of Thickness Variation on the Flapping Performance of Symmetric NACA Airfoils in Plunging Motion
Table 1
Values of for different .
| No. | Loc () | | | |
| 1 | 30.0% | 0.17211035378267 | 0.13867972442717 | 0.15458446304747 | 2 | 35.0% | 0.17211035378267 | 0.11758914339250 | 0.24333708636138 | 3 | 40.0% | 0.17211035378267 | 0.10417878455362 | 0.28842711913075 | 4 | 45.0% | 0.17211035378267 | 0.09353460035375 | 0.31733390835548 | 5 | 50.0% | 0.17211035378267 | 0.08244808744449 | 0.34181598126744 |
|
|