| contributor author | R. J. El Assar | |
| date accessioned | 2017-05-09T00:38:21Z | |
| date available | 2017-05-09T00:38:21Z | |
| date copyright | September, 1970 | |
| date issued | 1970 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-27367#510_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/143545 | |
| description abstract | A finite difference solution is presented for the laminar, compressible wake behind a flat plate at zero angle of attack. The solution of the boundary layer equations is carried out in the von Mises coordinate plane. A coordinate transformation which maps the infinite region into a finite one is also introduced. The accuracy and range of validity of the asymptotic and preasymptotic theories of Goldstein and Tollmien for the incompressible wake are discussed. The effect of the Mach number and initial conditions on the evolution of the wake is investigated. The analysis is applicable outside a trailing edge region of O(LRc −3/4 ) and for a constant density-viscosity product and Prandtl number unity. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Compressible Laminar Wake of a Thin Flat Plate | |
| type | Journal Paper | |
| journal volume | 92 | |
| journal issue | 3 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3425048 | |
| journal fristpage | 510 | |
| journal lastpage | 513 | |
| identifier eissn | 1528-901X | |
| keywords | Wakes | |
| keywords | Flat plates | |
| keywords | Prandtl number | |
| keywords | Boundary layers | |
| keywords | Equations | |
| keywords | Density | |
| keywords | Mach number AND Viscosity | |
| tree | Journal of Fluids Engineering:;1970:;volume( 092 ):;issue: 003 | |
| contenttype | Fulltext | |
