| contributor author | W. C. Chin | |
| date accessioned | 2017-05-08T23:06:12Z | |
| date available | 2017-05-08T23:06:12Z | |
| date copyright | March, 1979 | |
| date issued | 1979 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-26112#6_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/91832 | |
| description abstract | The inverse problem, which determines an airfoil geometry given some specified surface pressure, is considered in the subsonic, thin-airfoil limit. The full governing equations are expanded in powers of the thickness ratio and solved to second-order. The two sequential formulations contain free parameters, which are fixed by invoking “Kutta-type” conditions related to trailing edge closure. The correctness of the basic approach is demonstrated by using known classical examples for the simpler first-order problem. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | On the Design of Thin Subsonic Airfoils | |
| type | Journal Paper | |
| journal volume | 46 | |
| journal issue | 1 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3424530 | |
| journal fristpage | 6 | |
| journal lastpage | 8 | |
| identifier eissn | 1528-9036 | |
| keywords | Design | |
| keywords | Airfoils | |
| keywords | Pressure | |
| keywords | Equations | |
| keywords | Geometry | |
| keywords | Inverse problems AND Thickness | |
| tree | Journal of Applied Mechanics:;1979:;volume( 046 ):;issue: 001 | |
| contenttype | Fulltext | |
