Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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B-F-R Case, Euler Simulation, Mach 1.05´µÌ¹¹Ê×ØÅ½º¼CP: -0.78 -0.56 -0.42 -0.27 -0.13 0.02 0.16 0.31 0.45 0.60 0.74 0.89 1.03B-F-R-T Case, Euler Simulation, Mach 1.05´µÌ¹¹Ê¹Ì×ØÅ½º¼CP: -0.780 -0.567 -0.354 -0.142 0.071 0.284 0.497 0.700 0.900B-F-W-R-T Case, Euler Simulation, Mach 1.05Position of the cross sectional planeÓÓÑÔÐÜØÝº ÙÖº¿ÀÛ×ØÝ×ÙÖÔÖ××ÙÖÓÒØÓÙÖ×ØÅ½º¼ÓÖ××ÛØÒÖ×ÒÐÚÐ ´µÌ¹¹Ï¹Ê¹Ì×ØÅ½º¼CP: -0.78 -0.6 -0.42 -0.24 -0.06 0.12 0.3 0.48 0.66 0.84 1.02½¿
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Case 3: Mach 0.769, frequency 5 Hz.
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Case 3: Mach 0.769, frequency 5 Hz.
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P: 0.6 0.666667 0.733333 0.8 0.8666
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Aeroelastic Analysis of Aircraft with Control Surfaces ... - CFD4Aircraft

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