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. Fig, Representation of the evolution of the Mach number, torsion angle, the pitching moment coefficient, the flow separation region and the chordwise position of the shock at r/R = 0.915 section (HRPM), vol.22

, Representation of the evolution of the Mach number, torsion angle, the pitching moment coefficient, the flow separation region and the chordwise position of the shock at r/R = 0.915 section (MRPM), vol.23