39th Aerospace Sciences Meeting and Exhibit 2001
DOI: 10.2514/6.2001-1016
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Numerical study of leading-edge heat transfer under free-stream turbulence

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Cited by 6 publications
(6 citation statements)
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“…The existence of a threshold in disturbance amplitude is also consistent with earlier observations by Nagib and Hodson (1978) on the formation of vortex pair at the stagnation region of a bluff body subject to the impingement of wakes. Similar flow patterns as those shown in figure 6.3 and 6.4 also emerge in aforementioned experiments (Nagib and Hodson, 1978;Botcher and Wedemeyer, 1989) as well as numerical simulations (Xiong and Lele, 2001;Bae et al, 2003). The quantitative characterization of the flow fields in figure 6.4 in terms of the maximum wall normal disturbance velocity [umoxlj wall vorticity |a;,"| and heat transfer enhancement A/i//i are summarized in Table 6.1.…”
Section: Numerical Resultssupporting
confidence: 52%
See 1 more Smart Citation
“…The existence of a threshold in disturbance amplitude is also consistent with earlier observations by Nagib and Hodson (1978) on the formation of vortex pair at the stagnation region of a bluff body subject to the impingement of wakes. Similar flow patterns as those shown in figure 6.3 and 6.4 also emerge in aforementioned experiments (Nagib and Hodson, 1978;Botcher and Wedemeyer, 1989) as well as numerical simulations (Xiong and Lele, 2001;Bae et al, 2003). The quantitative characterization of the flow fields in figure 6.4 in terms of the maximum wall normal disturbance velocity [umoxlj wall vorticity |a;,"| and heat transfer enhancement A/i//i are summarized in Table 6.1.…”
Section: Numerical Resultssupporting
confidence: 52%
“…the streamwise velocity is a linear function of the streamwise coordinate x , and the wall normal velocity IS .ndependent of z. The flow structures induced by free-stream turbulence in a stagnation region are found to be qualitatively similar to those induced bv upstream organized disturbances (Xiong and Lele, 2001). The importance of cal simir'' r^^ uf ^"^ *''"" '^""" ^^^^"^'^ *^^«"eh direct numer- (2003) " ^ stagnation point flow by Bae, Lele, and Sung…”
Section: Introductionmentioning
confidence: 71%
“…the streamwise velocity is a linear function of the streamwise coordinate x, and the wall normal velocity is independent of x. The flow structures induced by free-stream turbulence in a stagnation region are found to be qualitatively similar to those induced by upstream organized disturbances (Xiong & Lele 2001). The importance of the disturbance length scale has been shown recently through direct numerical simulation of a turbulent stagnation point flow by Bae, Lele & Sung (2003).…”
Section: Introductionmentioning
confidence: 66%
“…Using numerical simulation of a swept Hiemenz boundary layer, Spalart (1989) found that, out of initial whitenoise disturbances, the most unstable disturbance-mode is the one with the same similarity form as the mean Hiemenz flow, an assumption made in the stability analysis mentioned above. The flow structures induced by free-stream turbulence in a stagnation region were found to be qualitatively similar to those induced by upstream organized disturbances (Xiong & Lele 2001). Bae, Lele & Sung (2000) showed that different length scales generate quite different flow patterns and in turn different heat transfer responses in a plane stagnation-point flow.…”
Section: Introductionmentioning
confidence: 69%