| contributor author | A. T. Olson | |
| date accessioned | 2017-05-09T01:38:25Z | |
| date available | 2017-05-09T01:38:25Z | |
| date copyright | March, 1974 | |
| date issued | 1974 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26853#21_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/164922 | |
| description abstract | Using Walz’s approximation method for boundary layer calculation, along with a one-dimensional treatment of the compressible inviscid core flow, discharge coefficients for small nozzle to pipe diameter ratios have been calculated. Discharge co-efficients calculated for the ASME long radius nozzle agree with those recommended by the ASME Power Test Code. In addition, experimental confirmation of an indicated Mach number effect has been achieved in a nozzle modified to minimize two-dimensional effects. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Nozzle Discharge Coefficients—Compressible Flow | |
| type | Journal Paper | |
| journal volume | 96 | |
| journal issue | 1 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3447088 | |
| journal fristpage | 21 | |
| journal lastpage | 24 | |
| identifier eissn | 1528-901X | |
| keywords | Nozzles | |
| keywords | Compressible flow | |
| keywords | Discharge coefficient | |
| keywords | Pipes | |
| keywords | Approximation | |
| keywords | Flow (Dynamics) | |
| keywords | Mach number AND Boundary layers | |
| tree | Journal of Fluids Engineering:;1974:;volume( 096 ):;issue: 001 | |
| contenttype | Fulltext | |
