Comparison of Laminar Separation Bubble Measurements on a Low Reynolds Number Airfoil in Three Facilities

By M. Ol, Brian McCauliffe, E. Hanff, U. Scholz, C. Kaehler. 2005

280 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Ocean Engineering

View Paper: https://www.semanticscholar.org/paper/ca62505b5f1cf2a6577bec2d869e097705e1b003

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In Aerospace Engineering

In Computational Mechanics

In Ocean Engineering

Citations in the corpus

The influence of airfoil kinematics on the formation of leading-edge vortices in bio-inspired flight (2009, unknown): “An attractive feature of the SD7003 profile is the substantial experimental database available in the open literature for the steady case provided in Selig et al. (1995) and Ol et al. (2005) as well as the unsteady case found in Nerger et al. (2003) and Lian et al. (2008).”
Dynamics of laminar separation bubbles at low-Reynolds-number aerofoils (2009, methodology): “These measurements were also discussed by Ol et al. (2005).”
Time-resolved and volumetric PIV measurements of a transitional separation bubble on an SD7003 airfoil (2008, methodology): “Ol et al. (2005), to define the transition onset.”
Discrete-vortex method with novel shedding criterion for unsteady aerofoil flows with intermittent leading-edge vortex shedding (2014, methodology): “More detail on the rig operation is given in Ol et al. (2009a) and Granlund, Ol & Bernal (2011), while the facility is discussed in Ol et al. (2005).”
High‐order discontinuous Galerkin spectral element methods for transitional and turbulent flow simulations (2014, background): “This airfoil has been subject of experimental [65, 66] and some computational investigations in the last years [67–69], most of them using implicit or explicit LES approaches.”
Unsteady force generation and vortex dynamics of pitching and plunging aerofoils (2012, unknown): “Given that the static stall angle of attack of SD7003 airfoil is approximately 11° [85], the shallow stall kinematic is expected to result in separation, reattachment, and laminar-to-turbulent transition at low Re.”
Shallow and deep dynamic stall for flapping low Reynolds number airfoils (2009, background): “Static stall in the present data set occurs at *11 , confirming prior results in the same facility with a larger model with a conventional static aft-mount static sting (Ol et al. 2005).”
On the Unsteady Behavior of the Flow around NACA 0012 Airfoil with Steady External Conditions at Re=1000 (2015, background): “For the design and control purpose of MAVs, the understanding of unsteady phenomena of low Reynolds numbers flows becomes important in last decades [4-6].”
Laminar-Turbulent Transition of a Low Reynolds Number Rigid or Flexible Airfoil (2006, methodology): “[40] predicted that the flow separates and reattaches further upstream.”