Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft

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17 Figure 1: Instantaneous flow showing the transition process with increasing Reynolds number (left); and time-averaged flow showing mean vortical substructures (right) [5] Figure 2: Magnitude of velocity measured by PIV over a slender delta wing showing the timeaveraged structured of vortex breakdown.
18 Figure 3: Spectrum of unsteady flow phenomena over delta wings as a function of dimensionless frequency [15] Figure 4: Scatter of vortex breakdown location in different facilities (from [14])
Page 1 and 2: Integrating CFD and Experiment in A
Page 3 and 4: Experimentalist’s requirements fo
Page 5 and 6: persistent discrepancy may be due t
Page 7 and 8: numbers significantly lower than th
Page 9 and 10: Heat flux measurements. Over the pa
Page 11 and 12: The measurements are made on select
Page 13 and 14: advantage that the signal is emitte
Page 15 and 16: 12. Mébarki, Y. and Mérienne, M.
Page 17 and 18: castellated nozzles entrained more
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
Page 29 and 30: 2 which include boundary layer and
Page 31 and 32: 4 not received much attention in th
Page 33 and 34: 6 Although a great deal of effort h
Page 35 and 36: 8 Computational simulations can con
Page 37 and 38: 10 separation location over rounded
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: 16 [31] Gursul, I., Proposed Mechan
Page 47 and 48: 20 Figure 7: Flow visualisation of
Page 49 and 50: Figure 11: Upper surface pressure d
Page 51 and 52: While the information presented in
Page 53 and 54: Figure 3 : DFR against Flap angle f
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Page 57 and 58: Figure 9 : Contours of Mach number,
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Page 77 and 78: Cs comparison at V=0.6 m/s Fig. 10.
Page 79 and 80: Investigation of Flow Turning in a
Page 81 and 82: duct as it approaches the blocker c
Page 83 and 84: Figure 1. Natural Blockage Thrust R
Page 85 and 86: Figure 7. Post-Exit rake Total Span
Page 87 and 88: Figure 11. Comparison of Static Pre
Page 89 and 90: 2.2 Data Aquired The Embedded Laser
Page 91 and 92: First, plots of the turbulent Reyno
Page 93 and 94: Particles seeding tube 3 m 1 m mode
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Page 97 and 98:
Figure 5: Influence of the pseudo t
Page 99 and 100:
Figure 7: Turbulent Reynolds' numbe
Page 101 and 102:
Figure 9: Turbulent Reynolds' numbe
Page 103 and 104:
Figure 11: Vortex Shedding cycle fo
Page 105 and 106:
Figure 13: Comparison with experime
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