论文信息 - Decay of Aircraft Vortices near the Ground - 字舞流文

Decay of Aircraft Vortices near the Ground

Milton E. Teske | Alan J. Bilanin | J. W. Barry | John W. Barry | M. Teske | A. Bilanin

[1] J. W. Barry,et al. FSCBG: An aerial spray dispersion model for predicting the fate of released material behind aircraft , 1993 .

[2] Milton E. Teske,et al. AGDISP: The Aircraft Spray Dispersion Model, Code Development and Experimental Validation , 1989 .

[3] Manoochehr Koochesfahani,et al. Initial acceleration effects on the flow field development around rapidly pitching airfoils , 1993 .

[4] Anjaneyulu Krothapalli,et al. Unsteady flow past an airfoil pitching at a constant rate , 1992 .

[5] Peter F. Lorber,et al. Airfoil dynamic stall at constant pitch rate and high Reynolds number , 1987 .

[6] Eric J. Jumper,et al. Lift-curve characteristics for an airfoil pitching at constant rate , 1986 .

[7] M. Francis,et al. Airfoil dynamic stall performance with large-amplitude motions , 1985 .

[8] Miguel R. Visbal,et al. On the formation and control of the dynamic stall vortex on a pitching airfoil , 1991 .

[9] Mukund Acharya,et al. Unsteady pressure field and vorticity production over a pitching airfoil , 1992 .

[10] M. E. Teske,et al. Vortex interactions and decay in aircraft wakes , 1977 .

[11] L. Carr. Progress in analysis and prediction of dynamic stall , 1988 .