Gust response of rigid and elastically mounted airfoils at a transitional Reynolds number
Author:
Funder
Air Force Office of Scientific Research
AFRL
ERDC
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference31 articles.
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2. Experimental small-amplitude self-sustained pitch-heave oscillations at transitional Reynolds numbers;Poirel;AIAA J.,2014
3. Computational aeroelastic simulations of self-sustained pitch oscillations of a NACA0012 at transitional Reynolds numbers;Poirel;J. Fluids Struct.,2011
4. On the role of flow transition in laminar separation flutter;Barnes;J. Fluids Struct.,2018
5. Vortex–body interactions;Rockwell;Annu. Rev. Fluid Mech.,1998
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