Affiliation:
1. Department of Mechanical Engineering, United States Naval Academy, Annapolis, MD 21402
Abstract
An experimental investigation has been carried out on a transitional boundary layer subject to high (initially 9%) freestream turbulence, strong acceleration (K=ν/Uw2dUw/dx as high as 9×10−6), and strong concave curvature (boundary layer thickness between 2% and 5% of the wall radius of curvature). Mean and fluctuating velocity as well as turbulent shear stress are documented and compared to results from equivalent cases on a flat wall and a wall with milder concave curvature. The data show that curvature does have a significant effect, moving the transition location upstream, increasing turbulent transport, and causing skin friction to rise by as much as 40%. Conditional sampling results are presented which show that the curvature effect is present in both the turbulent and nonturbulent zones of the transitional flow.
Reference28 articles.
1. Mayle, R. E.
, 1991, “The Role of Laminar-Turbulent Transition in Gas Turbine Engines,” ASME J. Turbomach., 113, pp. 509–537.
2. Go¨rtler, H.
, 1941, “Instabilita¨t Laminarer Grenzchichten an Konkaven Wa¨nder Gegenu¨ber Gewissen Dreidimensionalen Stro¨rungen,” Z. Angew. Math. Mech., 21, pp. 250–252 (see also NACA TM 1375, 1954).
3. Liepmann, H. W., 1943, “Investigations on Laminar Boundary Layer Stability and Transition on Curved Boundaries,” NACA Wartime Report W-87.
4. Floryan, J. M.
, 1991, “On the Go¨rtler Instability of Boundary Layers,” Prog. Aerosp. Sci., 28, pp. 235–271.
5. Saric, W. S.
, 1994, “Go¨rtler Vortices,” Annu. Rev. Fluid Mech., 26, pp. 379–409.
Cited by
21 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献