Aerodynamic Performance of a Scale-Model, Counterrotating Unducted FanSource: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004::page 579Author:T. J. Sullivan
DOI: 10.1115/1.2927696Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The aerodynamic performance of a scale-model, counterrotating unducted fan has been determined and the results are discussed herein. Experimental investigations were conducted using the scale-model propulsor simulator and uniquely shaped fan blades designed by the General Electric Company under contract to NASA. The blades, designed for a high disk loading at Mach 0.72, 35,000 ft altitude max climb condition, are aft-mounted on the simulator in a “pusher” configuration. Data are compared with analytical predictions at the design point and show good agreement.
keyword(s): Design , Disks AND Blades ,
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contributor author | T. J. Sullivan | |
date accessioned | 2017-05-08T23:33:59Z | |
date available | 2017-05-08T23:33:59Z | |
date copyright | October, 1990 | |
date issued | 1990 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28606#579_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/107683 | |
description abstract | The aerodynamic performance of a scale-model, counterrotating unducted fan has been determined and the results are discussed herein. Experimental investigations were conducted using the scale-model propulsor simulator and uniquely shaped fan blades designed by the General Electric Company under contract to NASA. The blades, designed for a high disk loading at Mach 0.72, 35,000 ft altitude max climb condition, are aft-mounted on the simulator in a “pusher” configuration. Data are compared with analytical predictions at the design point and show good agreement. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Aerodynamic Performance of a Scale-Model, Counterrotating Unducted Fan | |
type | Journal Paper | |
journal volume | 112 | |
journal issue | 4 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2927696 | |
journal fristpage | 579 | |
journal lastpage | 586 | |
identifier eissn | 1528-8900 | |
keywords | Design | |
keywords | Disks AND Blades | |
tree | Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004 | |
contenttype | Fulltext |