| contributor author | E. J. Hopkins | |
| date accessioned | 2017-05-09T01:37:27Z | |
| date available | 2017-05-09T01:37:27Z | |
| date copyright | September, 1974 | |
| date issued | 1974 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-26015#551_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/164366 | |
| description abstract | For hypersonic Mach numbers up to about 8, the virtual origin for turbulent skin-friction calculations is shown to be close to the beginning of boundary-layer transition. A simple relationship between the beginning and end of boundary-layer transition is presented. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Simple Methods for Determining the Virtual Origin of Turbulent Boundary Layers in Hypersonic Flow on Sharp-Edged Flat Plates | |
| type | Journal Paper | |
| journal volume | 41 | |
| journal issue | 3 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3423346 | |
| journal fristpage | 551 | |
| journal lastpage | 553 | |
| identifier eissn | 1528-9036 | |
| keywords | Boundary layer turbulence | |
| keywords | Flat plates | |
| keywords | Hypersonic flow | |
| keywords | Boundary layers | |
| keywords | Mach number | |
| keywords | Turbulence AND Skin friction (Fluid dynamics) | |
| tree | Journal of Applied Mechanics:;1974:;volume( 041 ):;issue: 003 | |
| contenttype | Fulltext | |
