Unsteady Aerodynamics of Rotorcraft in Ground Effect - Aerospace ...

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$(Performance \226 Class 1 Airplane Motions)$

Figure 14: Difference in Low Frequency Components of Side Force at Advance Ratios 0.03 and 0.08 - 14 - American Institute of Aeronautics and Astronautics Figure 15: Natural Frequency of Load Cell Side Force to a step disturbance.
Figure 17: Variation of Side Force and Sideward Center of Pressure with Advance Ratio IGE vs. OGE, 0° Yaw. Figure 16: Variation of Frequency Components with increasing Advance Ratios IGE. - 15 - American Institute of Aeronautics and Astronautics
Page 1 and 2: AIAA Paper 2004-2431, Fluid Dynamic
Page 3 and 4: III. Experiment description The exp
Page 5 and 6: 1. Experiment Setup The fuselage wa
Page 7 and 8: moments, with large intervals possi
Page 9 and 10: Figure 3: Rotor and Test Section Fi
Page 11 and 12: x 10 6 Hotwire IGE Adv 0.03 Peak fr
Page 13: Figure 12: Experimental Setup: Fuse
Page 17 and 18: Figure 20: Variation of Side Force

Unsteady Aerodynamics of Rotorcraft in Ground Effect - Aerospace ...

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