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Extraction of skin friction topology of turbulent wedges on a swept wing in transonic flow from surface temperature images
This paper describes a first-order approximate method of extracting the skin friction topology of turbulent wedges from temperature sensitive paint (TSP) images on a NASA Common Research Model with Natural Laminar Flow (CRM-NLF) wing at Mach 0.85 in the National Transonic Facility (NTF) for full-fli...
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Published in: | Experiments in fluids 2021-10, Vol.62 (10), Article 215 |
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Main Authors: | , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | This paper describes a first-order approximate method of extracting the skin friction topology of turbulent wedges from temperature sensitive paint (TSP) images on a NASA Common Research Model with Natural Laminar Flow (CRM-NLF) wing at Mach 0.85 in the National Transonic Facility (NTF) for full-flight Reynolds number testing. The extracted skin friction topology of a typical turbulent wedge exhibits the similarity in the distributions of the surface temperature, skin friction magnitude and skin friction divergence. The developed method computes a normalized skin friction field associated with a surface temperature variation superposed on a simple known base flow. The selection of the relevant parameters in the application of this method is discussed, including the base-flow power-law exponent, relative amplitude of the surface temperature variation to the base flow, Lagrange multiplier, spatial resolution, and filter size.
Graphic abstract
Surface temperature and skin friction fields of a typical turbulent wedge: (a) temperature, (b) skin friction magnitude, and (c) skin friction divergence. The color bar has no unit. |
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ISSN: | 0723-4864 1432-1114 |
DOI: | 10.1007/s00348-021-03305-5 |