Static performance of a 13.97 cm (5.5 inch) diameter model VTOL lift fan

Lowe, W. H.; Sanger, R. W.

oai:casi.ntrs.nasa.gov:19720016186

Static performance of a 13.97 cm (5.5 inch) diameter model VTOL lift fan

Authors: W. H. Lowe
R. W. Sanger
Publication date: 1972
Publisher

Abstract

A tip-turbine-driven fan of the type currently being used in wind tunnel tests of VTOL lift fan models was tested. Values of thrust, weight flow, exit total and static pressure, exit swirl angle, and turbine temperature drop were measured as a function of fan speed for several inlet and exit configurations. A standard fan performance map was also obtained

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Last time updated on 02/09/2017

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