Effect of throat heating on critical roughness and the stability of nozzle wall boundary layer

1998 ◽  
Author(s):  
R.-S. Lin ◽  
V. Iyer ◽  
M. Malik
AIAA Journal ◽  
1975 ◽  
Vol 13 (3) ◽  
pp. 307-314 ◽  
Author(s):  
W. D. HARVEY ◽  
P. C. STAINBACK ◽  
J. B. ANDERS ◽  
A. M. CARY

2009 ◽  
Vol 2009.62 (0) ◽  
pp. 43-44
Author(s):  
Yuuki OKUZONO ◽  
Fujio AKAGI ◽  
Youichi ANDO ◽  
Masato FURUKAWA ◽  
Sumio YAMAGUCHI

1971 ◽  
Vol 93 (4) ◽  
pp. 386-396 ◽  
Author(s):  
R. P. Dring

An analysis is presented which is a combination of existing momentum-integral equations and existing studies of profile shapes for incompressible three-dimensional turbulent boundary layers. These, along with a number of suitable refinements and assumptions, result in a solution technique which is particularly well suited for turbine end-wall boundary layer calculations. The solution gives the distribution of the boundary layer thickness and skewing over the end-wall as well as the amount and flux of total pressure deficit of the flow leaving the end-wall at the suction surface corner. The analysis also disclosed that a shear term which is normally neglected in the boundary layer approximations must in fact be retained, at least in approximate form, in order to insure the stability of the integral equations.


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