Heat-Flux Gauge Studies of Compressible Dynamic Stall
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[1] S. M. Mangalam,et al. A unique measurement technique to study laminar-separation bubble characteristics on an airfoil , 1987 .
[2] M. S. Chandrasekhara,et al. Competing Mechanisms of Compressible Dynamic Stall , 1998 .
[3] M. S. Chandrasekhara,et al. Design and development of a compressible dynamic stall facility , 1992 .
[4] M. S. Chandrasekhara,et al. Compressible Dynamic Stall Calculations Incorporating Transition Modeling for Variable Geometry Airfoils , 1998 .
[5] William E. Faller,et al. Pitch rate and Reynolds number effects on unsteady boundary-layer transition and separation , 1998 .
[6] Tim Lee,et al. Measurement of unsteady boundary layer developed on an oscillating airfoil using multiple hot-film sensors , 1998 .
[7] M. S. Chandrasekhara,et al. On the competing mechanisms of compressible dynamic stall , 1996 .
[8] S. S. Davis,et al. Measurements of discrete vortex noise in a closed-throat wind tunnel , 1975 .
[9] John W. Kiedaisch,et al. Investigation of incipient dynamic stall over pitching airfoils using hot-film sensors , 1997 .
[10] M. S. Chandrasekhara,et al. Reattachment studies of an oscillating airfoil dynamic stall flowfield , 1994 .
[11] Eli Livne,et al. Future of Airplane Aeroelasticity , 2003 .
[12] M. S. Chandrasekhara,et al. Reattachment studies of an oscillating airfoil dynamic stall flowfield , 1991 .
[13] D. Knight,et al. PARALLEL COMPUTATION OF THE 2-D NAVIER-STOKES FLOWFIELD OF A PITCHING AIRFOIL , 1995 .
[14] William E. Faller,et al. Unsteady separation processes and leading edge vortex precursors - Pitch rate and Reynolds number influences , 2000 .