contributor author | Siu Shing Tong | |
contributor author | W. T. Thompkins | |
date accessioned | 2017-05-08T23:15:34Z | |
date available | 2017-05-08T23:15:34Z | |
date copyright | April, 1983 | |
date issued | 1983 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26781#369_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/97109 | |
description abstract | A previously described, inviscid design technique has been substantially improved to allow the generation of either shock-free, weak-shock or low total pressure loss supersonic rotor cascade designs. Improvements have been introduced in inflow-outflow boundary conditions, imposition of geometric constraints and in shock pressure rise specifications. Calculation examples are presented for precompression type rotor designs. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | A Design Calculation Procedure for Shock-Free or Strong Passage Shock Turbomachinery Cascades | |
type | Journal Paper | |
journal volume | 105 | |
journal issue | 2 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3227425 | |
journal fristpage | 369 | |
journal lastpage | 376 | |
identifier eissn | 0742-4795 | |
keywords | Shock (Mechanics) | |
keywords | Design | |
keywords | Turbomachinery | |
keywords | Pressure | |
keywords | Rotors | |
keywords | Boundary-value problems | |
keywords | Cascades (Fluid dynamics) | |
keywords | Inflow AND Outflow | |
tree | Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002 | |
contenttype | Fulltext | |