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contributor authorD. N. So̸rensen
contributor authorResearch Scientist
contributor authorM. C. Thompson
contributor authorResearch Scientist
contributor authorJ. N. So̸rensen
date accessioned2017-05-09T00:02:43Z
date available2017-05-09T00:02:43Z
date copyrightJune, 2000
date issued2000
identifier issn0098-2202
identifier otherJFEGA4-27151#324_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123884
description abstractNumerical design optimization of the aerodynamic performance of axial fans is carried out, maximizing the efficiency in a design interval of flow rates. Tip radius, number of blades, and angular velocity of the rotor are fixed, whereas the hub radius and spanwise distributions of chord length, stagger angle, and camber angle are varied to find the optimum rotor geometry. Constraints ensure a pressure rise above a specified target and an angle of attack on the blades below stall. The optimization scheme is used to investigate the dependence of maximum efficiency on the width of the design interval and on the hub radius. [S0098-2202(00)01602-3]
publisherThe American Society of Mechanical Engineers (ASME)
titleToward Improved Rotor-Only Axial Fans—Part II: Design Optimization for Maximum Efficiency
typeJournal Paper
journal volume122
journal issue2
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.483260
journal fristpage324
journal lastpage329
identifier eissn1528-901X
keywordsDesign
keywordsOptimization
keywordsRotors
keywordsFans
keywordsFlow (Dynamics)
keywordsBlades AND Pressure
treeJournal of Fluids Engineering:;2000:;volume( 122 ):;issue: 002
contenttypeFulltext


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