Supersonic Separated Flow past a Cylindrical Obstacle on a Flat Plate

AIAA Journal ◽  
1984 ◽  
Vol 22 (5) ◽  
pp. 611-617 ◽  
Author(s):  
Oktay Ozcan ◽  
Maurice Holt
Keyword(s):  
Flat Plate ◽  
Separated Flow ◽  
Cylindrical Obstacle ◽  
Flow Past

Input-Output Analysis of a Separated Flow Past a Flat Plate

2019 ◽  
Author(s):  
Hao Zhang ◽  
Clarence W. Rowley ◽  
Wen Wu ◽  
Charles Meneveau ◽  
Rajat Mittal
Keyword(s):  
Flat Plate ◽  
Separated Flow ◽  
Input Output ◽  
Output Analysis ◽  
Input Output Analysis ◽  
Flow Past

NATURAL CONVECTION BOUNDARY LAYER FLOW PAST A FLAT PLATE OF FINITE DIMENSIONS

2012 ◽  
Vol 15 (6) ◽  
pp. 585-593
Author(s):  
M. Jana ◽  
S. Das ◽  
S. L. Maji ◽  
Rabindra N. Jana ◽  
S. K. Ghosh
Keyword(s):  
Boundary Layer ◽  
Natural Convection ◽  
Flat Plate ◽  
Boundary Layer Flow ◽  
Convection Boundary Layer ◽  
Flow Past ◽  
Convection Boundary ◽  
Layer Flow

Rarefied gas flow past a flat plate at zero angle of attack

2020 ◽  
Vol 32 (8) ◽  
pp. 087108
Author(s):  
A. A. Abramov ◽  
A. V. Butkovskii ◽  
O. G. Buzykin
Keyword(s):  
Flat Plate ◽  
Gas Flow ◽  
Rarefied Gas ◽  
Angle Of Attack ◽  
Rarefied Gas Flow ◽  
Flow Past

Separated Flow Past a Slender Delta Wing at Incidence

1973 ◽  
Vol 24 (2) ◽  
pp. 120-128 ◽  
Author(s):  
J E Barsby
Keyword(s):  
Delta Wing ◽  
Separated Flow ◽  
Leading Edge ◽  
Vortex Sheet ◽  
Simultaneous Equations ◽  
Delta Wings ◽  
Nested Iteration ◽  
Finite Difference Technique ◽  
Flow Past ◽  
Vortex Systems

SummarySolutions to the problem of separated flow past slender delta wings for moderate values of a suitably defined incidence parameter have been calculated by Smith, using a vortex sheet model. By increasing the accuracy of the finite-difference technique, and by replacing Smith’s original nested iteration procedure, to solve the non-linear simultaneous equations that arise, by a Newton’s method, it is possible to extend the range of the incidence parameter over which solutions can be obtained. Furthermore for sufficiently small values of the incidence parameter, new and unexpected results in the form of vortex systems that originate inboard from the leading edge have been discovered. These new solutions are the only solutions, to the author’s knowledge, of a vortex sheet leaving a smooth surface.Interest has centred upon the shape of the finite vortex sheet, the position of the isolated vortex, and the lift, and variations of these quantities are shown as functions of the incidence parameter. Although no experimental evidence is available, comparisons are made with the simpler Brown and Michael model in which all the vorticity is assumed to be concentrated onto an isolated line vortex. Agreement between these two models becomes very close as the value of the incidence parameter is reduced.

Separated flow noise of a flat plate at large attack angles

1983 ◽  
Vol 89 (3) ◽  
pp. 335-357 ◽  
Author(s):  
Y. Maruta ◽  
S. Kotake
Keyword(s):  
Flat Plate ◽  
Separated Flow ◽  
Flow Noise
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