Performance Measurement and Wake Characteristics of a Model Rotor in Axial Flight
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[1] A. T. Conlisk,et al. Interaction of Tip-Vortices in the Wake of a Two-Bladed Rotor in Axial Flight , 1998 .
[2] Fort F. Felker,et al. Reduction of Unsteady Recirculation in Hovering Model Helicopter Rotor Testing , 1987 .
[3] J. G. Leishman,et al. Challenges in Understanding the Vortex Dynamics of Helicopter Rotor Wakes , 1998 .
[4] Oktay Ozcan,et al. Cylinder-induced shock-wave boundary-layer interaction , 1992 .
[5] Vernon J. Rossow. Wake-vortex separation distances when flight-path corridors are constrained , 1996 .
[6] Narayanan Komerath,et al. Visualization and Measurement of the Tip Vortex Core of a Rotor Blade in Hover , 1988 .
[7] Wayne Johnson,et al. Performance results from a test of an S-76 rotor in the NASA Ames 80- by 120-foot wind tunnel , 1993 .
[8] Reinert H. G. Mu¨ller. Special Vortices at a Helicopter Rotor Blade , 1990 .
[9] N. Komerath,et al. Flowfield of a swept blade tip at high pitch angles , 1991 .
[10] H. M. Mcmahon,et al. Measurement of the Interaction Between a Rotor Tip Vortex and a Cylinder , 1990 .