... 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|