Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft

More documents

Recommendations

Info

Figure 9. Detail of <strong>CFD</strong> Model Geometry Figure 10. Velocity Vectors <strong>in</strong> the Thrust Reverser.
Figure 11. Comparison of Static Pressure Distribution on Bottom Wall. Figure 12. Comparison of Static Pressure Distribution on Top Wall.
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 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,
Page 59 and 60: ¥:97§Y©R¥e©H !V( H ¨9#f§e!"
Page 61 and 62: é¡êŒëWì¤í?î(ïeð±ñWòL
Page 63 and 64: Ó3×ÓnØ*Ù(Ú*Û+Ü ÝÞ#ß)ÝG
Page 65 and 66: 6‹wB6h67 C,7D4 ')(r,+.st/9:!/L£8
Page 67 and 68: ACBDsEutCIvwlxV^ c Q!Lkd_Q_SFM PQ_^
Page 69 and 70: Ç¹ºF»¼@½:¾¿_À!Á »_ÂÃk
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: Figure 7. Post-Exit rake Total Span
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
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
show all

Integrating CFD and Experiment in Aerodynamics - CFD4Aircraft

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?