Abstract
BUFFET 0 2 C N I CN T experimental results in Fig. Ib are incorrect according ONSET to a recent publication. The old, preliminary apparent Fig l Apparent damping of first wing-bending mode (Ref. 1). damping results and the final, correct ones are shown in Fig. 1. This explains the inability of the analysis, Eq. (27) and associated text, to predict the previously published damping increase before buffet onset. The present, corrected experimental results are in rather good agreement with _ predictions. Reference *Maby, D.G., Some Remarks on Buffeting, VKI Lecture Series _____ 1981-4 on Unsteady Airloads and Aeroelastic Problems in Separated Received April 8, 1981. and Transonic Flow, March 9-13, 1981, Von Karman Institute, Rhode 'Senior Consulting Engineer. Saint Geuese, Belgium.
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