SURVEY OF RESEARCH ON UNSTEADY AERODYNAMIC LOADING OF DELTA WINGS

For aeronautical applications there has been recent interest in accurately determining the aerodynamic forces and moments experienced by low-aspect-ratio wings performing transient maneuvers which go to angles of attack as high as 90°. Focusing on the delta planform with sharp leading edges, the paper surveys experimental and theoretical investigations dealing with the associated unsteady flow phenomena. For maximum angles above a value between 30 and 40°, flow details and airloads are dominated by hysteresis in the "bursting" instability of intense vortices which emanate from the leading edge. As examples of relevant test results, force and moment histories are presented for a model series with aspect ratios 1, 1·5 and 2. Influences of key parameters are discussed, notably those which measure unsteadiness. Comparisons are given with two theories: a paneling approximation that cannot capture bursting but clarifies other unsteady influences; and a simplied estimation scheme which uses measured bursting data. © 1991 Academic Press Limited.