Octant Analysis of the Reynolds Stresses in the Three Dimensional Turbulent Boundary Layer of a Prolate Spheroid
Abstract (Summary)
The Reynolds stresses in a three-dimensional turbulent
boundary layer were examined using octant analysis. The
representative flow was a pressure driven, three-dimensional
turbulent boundary layer on the leeside
(x/L=0.76-0.78, phi=105°-130°) of a 6:1 prolate spheroid at
10° angle of attack. The Reynolds number for the flow was
Re=4.2x10E+6. The LDV data of Chesnakas, Simpson, and Madden
(1994) were the basis of examination. This data set employed
a post-processing technique for refining the radial location
of the measurments. A least-squares fit of the Spalding wall
law was used to both correct the measurement locations and
estimate the wall shear stress. This paper presents a
previously unpublished assesment of the techinque. Octant
analysis was performed on the corrected data under
free-stream and wall-collateral coordinates. (The wall-collateral
coordinate system is aligned with the mean tangential
velocity in the buffer-layer.) The octant analysis led to
the development of a structural model that extends the
sweep/ejection process to three dimensions. Ejections and
sweeps produce w' through the same mechanism that produces
u'; they transport fluid across a spanwise velocity
gradient. The model's results remain consistent with
coordinate rotation. The model also describes the
asymmetries that evolve between ejections and sweeps with
spanwise fluctuations (w') of opposite sign. These
asymmetries cause non-zero u'w' and v'w' in the buffer
layer. Comparison of the two coordinate systems reveals
that wall-collateral coordinates provides a simpler
foundation for octant analysis. The sweep and ejection
octants maintain a nearly equal distribution of velocity
events throughout the buffer and lower log layers. Also, the
spanwise velocity profile monotonically decreases to a
constant value at the boundary layer edge, simplifying
application of the sweep/ejection model to spanwise
fluctuations. Comparison with other 3DTBL experiments
suggests that the wall-collateral coordinates are more
closely aligned with the quasi-streamwise vortex structures
than free-stream coordinates. The octant analysis also
reveals structural behavior consistent with the four
mechanisms revealed by the direct numerical simulation of
Sendstad and Moin (1992).
Bibliographical Information:
Advisor:Dr. William Devenport; Dr. Wayne Neu; Dr. Roger Simpson
School:Virginia Polytechnic Institute and State University
School Location:USA - Virginia
Source Type:Master's Thesis
Keywords:aerospace and ocean engineering
ISBN:
Date of Publication:11/12/1997