Tests at Subsonic Speeds on a Half-Wing with a Fan Engine Nacelle

Abstract

SUMMARY Flutter tests have been made on a half-wing model with a fan-engine nacelle attached by a pylon at an inboard section. The model was nominally rigid and flexibilities in pitch and roll were introduced at the root. Measurements were made of the flutter characteristics of the model at Mach numbers of 0.6 and 0.8 over a range of dynamic pressures using… (More)

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Cite this paper

@inproceedings{Drane1974TestsAS, title={Tests at Subsonic Speeds on a Half-Wing with a Fan Engine Nacelle}, author={D. A. Drane and G. B. Hutton}, year={1974} }