| contributor author | P. F. Maeder | |
| contributor author | H. U. Thommen | |
| date accessioned | 2017-05-09T00:18:40Z | |
| date available | 2017-05-09T00:18:40Z | |
| date copyright | December, 1961 | |
| date issued | 1961 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-25644#481_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/133056 | |
| description abstract | The simple linearized transonic flow theory as originally proposed by Oswatitsch and Keune [1] and by the present authors [2] is improved by considering and partially correcting its error. In this manner a theory which is easy to apply and which should be valid for a great number of smooth bodies is obtained. This improved theory predicts shock waves in the lower transonic regions. It is applied to a number of significant body and airfoil shapes and its predictions are compared with experiments and results of other theoretical investigations. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Linearized Transonic Flow About Slender Bodies at Zero Angle of Attack | |
| type | Journal Paper | |
| journal volume | 28 | |
| journal issue | 4 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3641772 | |
| journal fristpage | 481 | |
| journal lastpage | 490 | |
| identifier eissn | 1528-9036 | |
| keywords | Transonic flow | |
| keywords | Airfoils | |
| keywords | Shock waves | |
| keywords | Errors AND Shapes | |
| tree | Journal of Applied Mechanics:;1961:;volume( 028 ):;issue: 004 | |
| contenttype | Fulltext | |