Bottom Furrows and Estimated Currents in the Mississippi Delta Region

1983 ◽  
Vol 23 (01) ◽  
pp. 177-183 ◽  
Author(s):  
Charles E. Adams ◽  
David B. Prior ◽  
James M. Coleman

Summary A simple model of a neutrally buoyant, steady-state benthic boundary layer is used to examine the relationships between the dimensions of secondary roll vortices in the boundary layer and the spacing of a system of bottom furrows located offshore of the Mississippi Delta. The mean free-stream flow velocity predicted by the model, which creates the desired ratio between those two parameters, is an estimate of the free-stream current speed necessary for furrow erosion. In the absence of direct current measurements, such estimates are of value not only for offshore design but also for planning subsequent current measurement programs. Introduction In a recent paper, a system of bottom furrows located in a reentrant at the continental shelf edge in the Mississippi Delta region was described. These furrows and other recognized sedimentary bedforms indicate that bottom processes associated with near-bottom currents are active in the area. Direct observations of bottom currents, however, are scarce. Intensive petroleum exploration activities are being conducted in the potentially productive offshore Mississippi Delta area. Bottom activity and sediment movement are critical factors in the design and placement of oil and gas production and transportation facilities. The bottom furrows provide evidence of the general nature of the operative bottom processes. Using an existing boundary layer model and furrow geometry, it is possible to extract some quantitative information about the currents believed to be responsible for the furrows. These estimates can provide an important parametric input to design studies. In this paper, bottom furrows in the Mississippi Delta region are summarized briefly and their presence is attributed to a secondary circulation consisting of a system of longitudinal roll vortices. A benthic boundary layer model that accounts for the effects of stable stratification on boundary layer structure is used to extract quantitative information on near-bottom currents. Background The Mississippi Delta furrows became known initially as a result of a systematic mapping survey of the offshore Mississippi River delta area by high-frequency echo sounder, subbottom profiler, and side-scan sonar from 1977 through 1979. Closely spaced survey lines [900 ft (275 m)] allowed the furrow distribution to be mapped by sonographic mosaicking techniques. Subsequent work has documented the presence of similar highly localized features 50 miles (80 km) to the west in the Mississippi Canyon, A bathymetric influence on furrow location is suggested by the absence of these features in the intervening topographically uniform bottom area. Erosional furrows have been observed in a number of different marine environments. SPEJ P. 177^

2019 ◽  
Vol 1404 ◽  
pp. 012092
Author(s):  
M M Katasonov ◽  
V V Kozlov ◽  
A M Pavlenko ◽  
I A Sadovskii

Author(s):  
Heinz-Adolf Schreiber ◽  
Wolfgang Steinert ◽  
Bernhard Küsters

An experimental and analytical study has been performed on the effect of Reynolds number and free-stream turbulence on boundary layer transition location on the suction surface of a controlled diffusion airfoil (CDA). The experiments were conducted in a rectilinear cascade facility at Reynolds numbers between 0.7 and 3.0×106 and turbulence intensities from about 0.7 to 4%. An oil streak technique and liquid crystal coatings were used to visualize the boundary layer state. For small turbulence levels and all Reynolds numbers tested the accelerated front portion of the blade is laminar and transition occurs within a laminar separation bubble shortly after the maximum velocity near 35–40% of chord. For high turbulence levels (Tu > 3%) and high Reynolds numbers transition propagates upstream into the accelerated front portion of the CDA blade. For those conditions, the sensitivity to surface roughness increases considerably and at Tu = 4% bypass transition is observed near 7–10% of chord. Experimental results are compared to theoretical predictions using the transition model which is implemented in the MISES code of Youngren and Drela. Overall the results indicate that early bypass transition at high turbulence levels must alter the profile velocity distribution for compressor blades that are designed and optimized for high Reynolds numbers.


1997 ◽  
Vol 119 (3) ◽  
pp. 405-411 ◽  
Author(s):  
R. E. Mayle ◽  
A. Schulz

A theory is presented for calculating the fluctuations in a laminar boundary layer when the free stream is turbulent. The kinetic energy equation for these fluctuations is derived and a new mechanism is revealed for their production. A methodology is presented for solving the equation using standard boundary layer computer codes. Solutions of the equation show that the fluctuations grow at first almost linearly with distance and then more slowly as viscous dissipation becomes important. Comparisons of calculated growth rates and kinetic energy profiles with data show good agreement. In addition, a hypothesis is advanced for the effective forcing frequency and free-stream turbulence level that produce these fluctuations. Finally, a method to calculate the onset of transition is examined and the results compared to data.


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