
Repeatbility of lift, drag, and moment coefficients(Ma = 0.85,Re = 4.7×106)
Figures of the Article
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Plane view of CAE-AVM model (unit: mm)
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Wind tunnel test model of CAE-AVM
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Distribution of pressure measurement groove on the wing
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Thermal insulation coating on the wing surface
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Fluorescent markers on the lower wing surfaceof CAE-AVM model
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Model on the Z sting support
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Model in the support interference correction test with and without dummy support
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Repeatbility of lift, drag, and moment coefficients(Ma = 0.85,Re = 4.7×106)
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Repeatbility of pressure coefficients (Ma = 0.85,Re = 4.7×106)
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Comparison of pressure coefficients between numerical simulation and wind tunnel tests
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Comparisons of force and torque coefficients of BW before and after correction
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Comparison of wind tunnel test results between fixed and free transition
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Bending and twist deformations of wing and horizontal tail
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Influence of fluorescent markers on wind tunnel test results (Ma = 0.85, Re = 4.7×106)
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Lift and drag coefficients of CAE-AVM BW at different Mach numbers
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Oil flow test results at different Mach numbers when the lift coefficient is 0.5
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