Self-sustained shock oscillations on airfoils at transonic speeds

By B. Lee. 2001

359 citations recorded by the source corpus.

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

Low-Frequency Unsteadiness of Shock Wave/Turbulent Boundary Layer Interactions (2014, background): “Lee (2001) reviewed work on SBLIs on transonic airfoils, which differs in many ways from higher–Mach number interactions owing to the ability of acoustic waves to travel upstream and influence the interaction.”
Origin of transonic buffet on aerofoils (2007, background): “A number of empirical criteria have been proposed for predicting the onset of buffeting flow (see, for example, the review of Lee 2001).”
Some physical aspects of shock wave/boundary layer interactions (2009, background): “This is probably the case of transonic buffeting for which, according to classical interpretations, there is an acoustic feedback between the flow at the trailing edge of the profile and the shock wave [17].”
Space and time organization in a shock-induced separated boundary layer (2006, background): “The main characteristics of this interaction have been obtained (see most classical references in Delery & Marvin (1986) and Smits & Dussauge (1996) and in more recent reviews Dolling (2001), Lee (2001) for example.”
Stability, Receptivity, and Sensitivity Analyses of Buffeting Transonic Flow over a Profile (2015, background): “On the contrary, as also shown byother studies [5,7], the buffet frequency is sensitive to the upstream Mach number.”