Boundary-Layer Transition on an Axisymmetric Body at Incidence at Mach 1.2

AIAA Journal ◽  
2006 ◽  
Vol 44 (5) ◽  
pp. 973-980 ◽  
Author(s):  
Hiroki Sugiura ◽  
Naoko Tokugawa ◽  
Yoshine Ueda
Keyword(s):  
Boundary Layer ◽  
Axisymmetric Body ◽  
Boundary Layer Transition ◽  
Layer Transition

Smoke Visualization of Boundary-Layer Transition on a Spinning Axisymmetric Body

AIAA Journal ◽  
1981 ◽  
Vol 19 (12) ◽  
pp. 1607-1608 ◽  
Author(s):  
T. J. Mueller ◽  
R. C. Nelson ◽  
J. T. Kegelman ◽  
M. V. Morkovin
Keyword(s):  
Boundary Layer ◽  
Axisymmetric Body ◽  
Boundary Layer Transition ◽  
Layer Transition ◽  
Smoke Visualization

Laminar boundary-layer transition on a heated underwater body

1984 ◽  
Vol 144 ◽  
pp. 79-101 ◽  
Author(s):  
Gerald C. Lauchle ◽  
G. B. Gurney
Keyword(s):  
Boundary Layer ◽  
Reynolds Number ◽  
Free Stream ◽  
Total Concentration ◽  
Heated Surface ◽  
Axisymmetric Body ◽  
The Body ◽  
Boundary Layer Transition ◽  
Layer Transition ◽  
Maximum Heat

A large (3.05 m long × 0.32 m diameter) heated-surface, axisymmetric body, designed for transition research in a 1.22 m diameter water tunnel is described. Boundary-layer transition data are presented as functions of the heating power supplied to the body and the total concentration of free-stream particulate matter in the water. Body surface temperatures range from 0 to 25°C over the ambient water temperature, and the total heat supplied ranges from 0 to 93.3 kW. Transition-arclength Reynolds numbers are found to vary from 4.5 × 106 for the body operating cold to 3.64 × 107 for the maximum heat level considered. The concentration of free-stream particles is shown to affect the transition Reynolds number. These particles range in diameter from 10 to 70 μm and their concentration ranges from less than 5 to 198 particles per cm3. The decrease in transition Reynolds number due to to the higher concentration of particles is of order 30%.

EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF BOUNDARY LAYER TRANSITION ON BLUNTED CONES AT SUPERSONIC FLOW

2010 ◽  
Vol 40 (3) ◽  
pp. 309-319 ◽  
Author(s):  
V. N. Brazhko ◽  
A. V. Vaganov ◽  
N. A. Kovaleva ◽  
N. P. Kolina ◽  
I. I. Lipatov
Keyword(s):  
Boundary Layer ◽  
Supersonic Flow ◽  
Boundary Layer Transition ◽  
Layer Transition ◽  
Numerical Investigations

Automatic control of laminar boundary-layer transition

AIAA Journal ◽  
1997 ◽  
Vol 35 ◽  
pp. 85-90
Author(s):  
P. A. Nelson ◽  
M. C. M. Wright ◽  
J.-L. Rioual
Keyword(s):  
Boundary Layer ◽  
Automatic Control ◽  
Laminar Boundary Layer ◽  
Boundary Layer Transition ◽  
Layer Transition
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