| contributor author | A. Platt | |
| contributor author | J. F. Norbury | |
| date accessioned | 2017-05-08T23:12:17Z | |
| date available | 2017-05-08T23:12:17Z | |
| date copyright | September, 1963 | |
| date issued | 1963 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-27251#392_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/95212 | |
| description abstract | A description is given of an electrolytic tank which was constructed for measuring the lift of aerofoils when boundary layer effects are considered. The associated electrical circuits for measurement of potential and potential gradient are given. Experiments were carried out on a single Piercy 12/40 aerofoil, and the measured lift agreed with wind tunnel observations within 1 percent. It is concluded that the electrolytic tank may be a useful tool in application to such problems. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Measurement of the Effects of Viscosity on Aerofoil Lift Using the Electrolytic Tank | |
| type | Journal Paper | |
| journal volume | 85 | |
| journal issue | 3 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3656619 | |
| journal fristpage | 392 | |
| journal lastpage | 399 | |
| identifier eissn | 1528-901X | |
| keywords | Viscosity | |
| keywords | Airfoils | |
| keywords | Boundary layers | |
| keywords | Circuits | |
| keywords | Gradients AND Wind tunnels | |
| tree | Journal of Fluids Engineering:;1963:;volume( 085 ):;issue: 003 | |
| contenttype | Fulltext | |
