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NASA NTRS · 19790016849

Design study and performance analysis of a high-speed multistage variable-geometry fan for a variable cycle engine

Abstract

A design technology study was performed to identify a high speed, multistage, variable geometry fan configuration capable of achieving wide flow modulation with near optimum efficiency at the important operating condition. A parametric screening study of the front and rear block fans was conducted in which the influence of major fan design features on weight and efficiency was determined. Key design parameters were varied systematically to determine the fan configuration most suited for a double bypass, variable cycle engine. Two and three stage fans were considered for the front block. A single stage, core driven fan was studied for the rear block. Variable geometry concepts were evaluated to provide near optimum off design performance. A detailed aerodynamic design and a preliminary mechanical design were carried out for the selected fan configuration. Performance predictions were made for the front and rear block fans.

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BibTeXRIS

Sullivan, T. J., Parker, D. E.. 1979-03-01. Design study and performance analysis of a high-speed multistage variable-geometry fan for a variable cycle engine. https://ntrs.nasa.gov/citations/19790016849

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