dc.contributor.author |
Tuling, S
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|
dc.contributor.author |
Vallabh, Bhavya
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dc.contributor.author |
Morelli, Mauro F
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dc.date.accessioned |
2016-10-13T13:32:59Z |
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dc.date.available |
2016-10-13T13:32:59Z |
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dc.date.issued |
2015-04 |
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dc.identifier.citation |
Tuling, S., Vallabh, B. and Morelli, M.F. 2015. Compressibility effects for the AGARD-B model. Aeronautical Journal, 119 (4139), pp 543-552 |
en_US |
dc.identifier.issn |
0001-9240 |
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dc.identifier.uri |
http://aerosociety.com/News/Publications/Aero-Journal/Online/3024/Compressibility-effects-for-the-AGARDB-model
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|
dc.identifier.uri |
http://hdl.handle.net/10204/8824
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dc.description |
Copyright: 2015 Cambridge University Press. Due to copyright restrictions, the attached PDF file only contains the abstract of the full text item. For access to the full text item, please consult the publisher's website. The definitive version of the work is published in Aeronautical Journal, Vol. 119(4139), pp 543-552. |
en_US |
dc.description.abstract |
A numerical study of the flow topologies over the 60° delta wing of the AGARD-B model at Mach 0·80 has revealed that vortex bursting occurs between 13°-15° angle-of-attack, while vortex separation occurs above 18°. These aerodynamic features have been identified as additional comparison criteria which need to be replicated for facilities using the model for calibration or inter-tunnel comparison purposes. The numerical simulations were performed using ANSYS Fluent V13, a structured mesh with near wall treatment and the Spalart-Allmaras and - SST turbulence models, and validated experimentally in a 5' × 5' transonic facility. Other aspects not previously identified or studied are firstly a recovery shock between the primary and secondary vortex that exists only when vortex bursting occurs, and secondly the lack of a shock between the wing and vortex when the flow topology corresponds to the centreline shock region as observed in other studies. |
en_US |
dc.language.iso |
en |
en_US |
dc.publisher |
Cambridge University Press |
en_US |
dc.relation.ispartofseries |
Worklist;15536 |
|
dc.subject |
Advisory Group for Aeronautical Research and Development |
en_US |
dc.subject |
AGARD |
en_US |
dc.subject |
AGARD B-model |
en_US |
dc.subject |
SST turbulence models |
en_US |
dc.title |
Compressibility effects for the AGARD-B model |
en_US |
dc.type |
Article |
en_US |
dc.identifier.apacitation |
Tuling, S., Vallabh, B., & Morelli, M. F. (2015). Compressibility effects for the AGARD-B model. http://hdl.handle.net/10204/8824 |
en_ZA |
dc.identifier.chicagocitation |
Tuling, S, Bhavya Vallabh, and Mauro F Morelli "Compressibility effects for the AGARD-B model." (2015) http://hdl.handle.net/10204/8824 |
en_ZA |
dc.identifier.vancouvercitation |
Tuling S, Vallabh B, Morelli MF. Compressibility effects for the AGARD-B model. 2015; http://hdl.handle.net/10204/8824. |
en_ZA |
dc.identifier.ris |
TY - Article
AU - Tuling, S
AU - Vallabh, Bhavya
AU - Morelli, Mauro F
AB - A numerical study of the flow topologies over the 60° delta wing of the AGARD-B model at Mach 0·80 has revealed that vortex bursting occurs between 13°-15° angle-of-attack, while vortex separation occurs above 18°. These aerodynamic features have been identified as additional comparison criteria which need to be replicated for facilities using the model for calibration or inter-tunnel comparison purposes. The numerical simulations were performed using ANSYS Fluent V13, a structured mesh with near wall treatment and the Spalart-Allmaras and - SST turbulence models, and validated experimentally in a 5' × 5' transonic facility. Other aspects not previously identified or studied are firstly a recovery shock between the primary and secondary vortex that exists only when vortex bursting occurs, and secondly the lack of a shock between the wing and vortex when the flow topology corresponds to the centreline shock region as observed in other studies.
DA - 2015-04
DB - ResearchSpace
DP - CSIR
KW - Advisory Group for Aeronautical Research and Development
KW - AGARD
KW - AGARD B-model
KW - SST turbulence models
LK - https://researchspace.csir.co.za
PY - 2015
SM - 0001-9240
T1 - Compressibility effects for the AGARD-B model
TI - Compressibility effects for the AGARD-B model
UR - http://hdl.handle.net/10204/8824
ER -
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en_ZA |