Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft

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Bibliography 1. Berton, E. Favier, D., and Maresca., C, “Embedded L.V. Methodology for Boundary-Layer Measurements on Oscillating Models”, Proceedings of the Twenty-Eight Fluid Dynamics Conference, AIAA, AIAA paper 97/1832, Snowmass, June 1997. 2. Barakos, G.N., ''Study of Unsteady Aerodynamics Phenomena using advanced turbulence closures'', PhD thesis, UMIST, 1999. 3. Brandsma, F.J., Kok, J.C., Dol, H.S. and Elsenaar, A., ''Leading edge vortex flow computations and comparison with DNW-HST wind tunnel data''. RTO/AVT Vortex Flow Symposium, Loen, Norway, 2001.
Particles seeding tube 3 m 1 m model pitching Fore-and-aft U ∞ 0,5 m oscillating devices Laser source optical fibers Figure 1: S2L low speed wind-tunnel, Experimental set-up
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Integrating CFD and Experiment in A
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Experimentalist’s requirements fo
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persistent discrepancy may be due t
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numbers significantly lower than th
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Heat flux measurements. Over the pa
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The measurements are made on select
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advantage that the signal is emitte
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12. Mébarki, Y. and Mérienne, M.
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castellated nozzles entrained more
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Axisymmetric Regular Convergent Div
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Figure 5: Typical instantaneous PIV
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Figure 8: Streamwise Velocity Profi
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1.25 CFD (SKW PRESTO) Experimental
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5 Conclusions In this paper we have
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2 which include boundary layer and
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4 not received much attention in th
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6 Although a great deal of effort h
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8 Computational simulations can con
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10 separation location over rounded
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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
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
Page 55 and 56: Figure 7 shows a series of plots of
Page 57 and 58: Figure 9 : Contours of Mach number,
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Page 71 and 72: yaw angle. Also, extreme value coef
Page 73 and 74: 0.9 Cs vs yaw angle Side force coef
Page 75 and 76: Fig. 5. Grid block structure around
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: First, plots of the turbulent Reyno
Page 95 and 96: 000000000 MEASUREM ENT S MEASUREM E
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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