The effects of trailing vorticity on the flow through highly loaded cascades
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[1] J. Mccune,et al. Three-dimensional flow in transonic axial compressor blade rows , 1974 .
[2] S. Lang,et al. An Introduction to Fourier Analysis and Generalised Functions , 1959 .
[3] James E. McCune,et al. Lifting-line theory for subsonic axial compressor rotors , 1972 .
[4] J. Mccune,et al. Three-dimensional vortex theory for axial compressor blade rows at subsonic and transonic speeds , 1970 .
[5] J. Mccune. The Transonic Flow Field of an Axial Compressor Blade Row , 1958 .
[6] Olufemi Okurounmij,et al. Lifting Surface Theory of Axial Compressor Blade Rows: Part 11-Transonic Compressor , 1974 .
[7] J. Mccune. A Three Dimensional Theory of Axial Compressor Blade Rows - Application in Subsonic and Supersonic Flows , 1958 .
[8] K. T. Whitby,et al. Fluid mechanics of the laminar flow aerosol impactor , 1974 .
[9] H. Reissner,et al. On the Vortex Theory of the Screw Propeller , 1937 .
[10] W. Hawthorne,et al. Some Exact Solutions of the Flow Through Annular Cascade Actuator Discs , 1950 .