| contributor author | R. Y. Chen | |
| contributor author | J. C. Williams | |
| date accessioned | 2017-05-09T00:16:54Z | |
| date available | 2017-05-09T00:16:54Z | |
| date copyright | June, 1969 | |
| date issued | 1969 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-25889#146_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/132168 | |
| description abstract | A supersonic low-density gas stream produced in a supersonic nozzle was passed through a circular tube in which the transition from supersonic to subsonic flow took place. Static pressure distributions along the tube (and nozzle) and impact pressure distributions across the tube at several stations were measured to determine the nature of this transition. The impact pressure distributions were used, together with the local static pressure, to infer Mach number and velocity profiles in the tube. When the pressure distributions and center-line Mach number distributions are considered together, one obtains a fairly clear picture of the processes involved in the transition from supersonic to subsonic flow at low Reynolds numbers. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | On Transition From Supersonic to Subsonic Flow at Low Reynolds Numbers in a Tube | |
| type | Journal Paper | |
| journal volume | 36 | |
| journal issue | 2 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3564601 | |
| journal fristpage | 146 | |
| journal lastpage | 150 | |
| identifier eissn | 1528-9036 | |
| keywords | Reynolds number | |
| keywords | Subsonic flow | |
| keywords | Pressure | |
| keywords | Mach number | |
| keywords | Nozzles AND Density | |
| tree | Journal of Applied Mechanics:;1969:;volume( 036 ):;issue: 002 | |
| contenttype | Fulltext | |
