The effects of adverse pressure gradients on momentum and thermal structures in transitional boundary layers. Part 2: Fluctuation quantities
- Clemson Univ., SC (United States). Dept. of Mechanical Engineering
The effects of adverse pressure gradients on the thermal and momentum characteristics of a heated transitional boundary layer were investigated with free-stream turbulence ranging from 0.3 to 0.6 percent. Boundary layer measurements were conducted for two constant-K cases, K1 = {minus}0.51 {times} 10{sup {minus}6} and K2 = {minus}1.05 {times} 10{sup {minus}6}. The fluctuation quantities, u{prime}, v{prime}, t{prime}, the Reynolds shear stress ({ovr uv}), and the Reynolds heat fluxes ({ovr vt} and {ovr ut}) were measured. In general, u{prime}/U{sub {infinity}}, v{prime}/U{sub {infinity}}, and {ovr vt} have higher values across the boundary layer for the adverse pressure-gradient cases than they do for the baseline case (K = 0). The development of v{prime} for the adverse pressure gradients was more actively involved than that of the baseline. In the early transition region, the Reynolds shear stress distribution for the K2 case showed a near-wall shear developed at Y{sup +} = 70. For the baseline case, however, the maximum turbulent shear in the transition region was generated at Y{sup +} = 70, and no near-wall high-shear region was seen. Stronger adverse pressure gradients appear to produce more uniform and higher t{prime} in the near-wall region (Y{sup +} < 20) in both transitional and turbulent boundary layers. The instantaneous velocity signals did not show any clear turbulent/nonturbulent demarcations in the transition region. Increasingly stronger adverse pressure gradients seemed to produce large nonturbulent unsteadiness (or instability waves) at a similar magnitude as the turbulent spots could not be identified visually or through conventional conditional-sampling schemes. In addition, the streamwise evolution of eddy viscosity, turbulent thermal diffusivity, and Pr{sub t} are also presented.
- Sponsoring Organization:
- USDOE
- OSTI ID:
- 404411
- Report Number(s):
- CONF-950629-; ISSN 0889-504X; TRN: IM9653%%13
- Journal Information:
- Journal of Turbomachinery, Vol. 118, Issue 4; Conference: 40. International gas turbine and aeroengine congress and exposition, Houston, TX (United States), 5-8 Jun 1995; Other Information: PBD: Oct 1996
- Country of Publication:
- United States
- Language:
- English
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