Flowfield Model for a Rectangular Planform Wing beyond Stall
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[1] M. J. Lighthill,et al. Oscillating Airfoils at High Mach Number , 1953 .
[2] R. J. Kind,et al. Stability derivatives of sharp wedges in viscous hypersonic flow. , 1966 .
[3] V. V. Sychev. Three-dimensional hypersonic gas flow past slender bodies at high angles of attack , 1960 .
[4] Lars E. Ericsson,et al. Viscous and Elastic Perturbation Effects on Hypersonic Unsteady Airfoil Aerodynamics , 1977 .
[5] J. B. Barlow,et al. The effects of leading edge modifications on the post-stall characteristics of wings , 1980 .
[6] J. P. Appleton. Aerodynamic pitching derivatives of a wedge in hypersonic flow , 1964 .
[7] Wai How Hui,et al. Stability of oscillating wedges and caret wings in hypersonic and supersonic flows. , 1969 .
[8] K. J. Orlik-Rueckemann. Effect of Wave Reflections on the Unsteady Hypersonic Flow over a Wedge , 1966 .
[9] T. W. Feistel,et al. Reduction of Stall-Spin Entry Tendencies Through Wing Aerodynamic Design , 1976 .