Manual on Aeroelasticity

Manual on Aeroelasticity

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... as v increases. The subsonic theoretical curves were obtained by the method of Reference 46 for v - 0 and by that of Reference 44 for ... Emerson and Robinson91 measured the pitching damping for an unswept tapered wing of aspect ratio 3 for M = 0.6 ... 6.3 Delta Wings Most experimental work with these planforms consists of measurements for rigid pitching, in particular of the damping derivative.

Title:Manual on Aeroelasticity
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development. Structures and Materials Panel, W. P. Jones
Publisher: - 1960

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