Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft
Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft
21 Figure 9: RMS value of fluctuating velocity together with the surface streamline pattern obtained from velocity measurements close to the wing surface. Figure 10: Interaction of multiple vortices originating from strake and wing, showing coiling-up and vortex breakdown.
Figure 11: Upper surface pressure distribution and roll history from Euler simulations of the wing rock phenomenon 22
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- Page 7 and 8: numbers significantly lower than th
- Page 9 and 10: Heat flux measurements. Over the pa
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- Page 15 and 16: 12. Mébarki, Y. and Mérienne, M.
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- Page 19 and 20: Axisymmetric Regular Convergent Div
- Page 21 and 22: Figure 5: Typical instantaneous PIV
- Page 23 and 24: Figure 8: Streamwise Velocity Profi
- Page 25 and 26: 1.25 CFD (SKW PRESTO) Experimental
- Page 27 and 28: 5 Conclusions In this paper we have
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- Page 31 and 32: 4 not received much attention in th
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- Page 35 and 36: 8 Computational simulations can con
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- Page 39 and 40: 12 3.7 Vortex / flexible wing inter
- Page 41 and 42: 14 [8] Mitchell, A.M. and Molton, P
- Page 43 and 44: 16 [31] Gursul, I., Proposed Mechan
- Page 45 and 46: 18 Figure 3: Spectrum of unsteady f
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21<br />
Figure 9: RMS value of fluctuat<strong>in</strong>g velocity together with the surface streaml<strong>in</strong>e pattern obta<strong>in</strong>ed<br />
from velocity measurements close to the w<strong>in</strong>g surface.<br />
Figure 10: Interaction of multiple vortices orig<strong>in</strong>at<strong>in</strong>g from strake <strong>and</strong> w<strong>in</strong>g, show<strong>in</strong>g coil<strong>in</strong>g-up <strong>and</strong><br />
vortex breakdown.
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