contributor author | Karl Kovach | |
contributor author | D. M. Sandercock | |
date accessioned | 2017-05-09T01:08:47Z | |
date available | 2017-05-09T01:08:47Z | |
date copyright | July, 1961 | |
date issued | 1961 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26617#303_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/155056 | |
description abstract | A five-stage axial-flow compressor with all rotors operating with transonic relative inlet Mach numbers was designed as a research vehicle at the Lewis Research Center in 1952. The compressor was designed and tested as a component of a turbojet engine. This paper summarizes the research work done on this compressor including the aerodynamic design and detailed performance characteristics. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Aerodynamic Design and Performance of Five-Stage Transonic Axial-Flow Compressor | |
type | Journal Paper | |
journal volume | 83 | |
journal issue | 3 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3673192 | |
journal fristpage | 303 | |
journal lastpage | 320 | |
identifier eissn | 0742-4795 | |
keywords | Compressors | |
keywords | Design | |
keywords | Axial flow | |
keywords | Turbojets | |
keywords | Performance characterization | |
keywords | Mach number | |
keywords | Engines | |
keywords | Rotors AND Vehicles | |
tree | Journal of Engineering for Gas Turbines and Power:;1961:;volume( 083 ):;issue: 003 | |
contenttype | Fulltext | |