Evaluation of Assumed-Transition-Point Criterion in Context of Reynolds-Averaged Simulations Around Lighter-Than-Air Vehicles
DSpace at IIT Bombay
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Title |
Evaluation of Assumed-Transition-Point Criterion in Context of Reynolds-Averaged Simulations Around Lighter-Than-Air Vehicles
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Creator |
SUMAN, S
LAKSHMIPATHY, S PANT, RS |
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Subject |
SHAPE OPTIMIZATION
AIRSHIP BODIES |
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Description |
In this work, the performance of the assumed-transition-point criterion, in conjunction with Reynolds-averaged Navier Stokes simulations is evaluated over the hull of a lighter-than-air vehicle. The evaluation is performed by comparing the Reynolds-averaged Navier Stokes computations of drag, lift, and moment coefficients against those measured in experiments where 1) transition is forced to occur (forced-transition case) and 2) transition is allowed to occur naturally (free-transition case). It was found that by using the assumed-transition-point criterion Reynolds-averaged Navier Stokes computations satisfactorily recover the drag coefficient both at zero angle of attack and nonzero angles of attack up to five degrees when compared against the forced-transition case. However, irrespective of the location of the assumed transition point, Reynolds-averaged Navier Stokes fails to recover the experimentally observed values of the force and moment coefficients for the free-transition case. At this point, it is not clear if this failure is attributable to the assumed-transition-point criterion or to the Reynolds-averaged Navier Stokes framework itself. A similar systematic evaluation with more scale resolving computational fluid dynamics methods (large eddy simulation or bridging methods) may be helpful in ascertaining the reason of this failure.
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Publisher |
AMER INST AERONAUTICS ASTRONAUTICS
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Date |
2014-10-14T17:21:36Z
2014-10-14T17:21:36Z 2013 |
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Type |
Article; Proceedings Paper
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Identifier |
JOURNAL OF AIRCRAFT, 50(2)450-456
http://dx.doi.org/10.2514/1.C031880 http://dspace.library.iitb.ac.in/jspui/handle/100/14555 |
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Language |
en
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