Preliminary results from an experimental investigation of nozzle wall boundary layer at Mach numbers ranging from 27 to 47

1969 ◽  
Author(s):  
J. KEMP, JR. ◽  
A. SREEKANTH
Keyword(s):  
Boundary Layer ◽  
Experimental Investigation ◽  
Nozzle Wall ◽  
Preliminary Results ◽  
Wall Boundary Layer ◽  
Wall Boundary ◽  
Mach Numbers

Nozzle Wall Boundary-Layer Transition and Freestream Disturbances at Mach 5

AIAA Journal ◽  
1975 ◽  
Vol 13 (3) ◽  
pp. 307-314 ◽  
Author(s):  
W. D. HARVEY ◽  
P. C. STAINBACK ◽  
J. B. ANDERS ◽  
A. M. CARY
Keyword(s):  
Boundary Layer ◽  
Boundary Layer Transition ◽  
Nozzle Wall ◽  
Layer Transition ◽  
Wall Boundary Layer ◽  
Wall Boundary

An accurate experimental investigation of the shock-tube end-wall boundary layer in argon

1980 ◽  
Vol 23 (6) ◽  
pp. 799-803 ◽  
Author(s):  
A. Hirschberg ◽  
W.H.H. van Heugten ◽  
J.F.H. Willems ◽  
M.E.H. van Dongen
Keyword(s):  
Boundary Layer ◽  
Experimental Investigation ◽  
Shock Tube ◽  
Wall Boundary Layer ◽  
Wall Boundary ◽  
End Wall

B11 Effect of Nozzle-Wall Boundary Layer on Stable Formation of Vortex ring Induced by a Pulsatile Jet Flow

2009 ◽  
Vol 2009.62 (0) ◽  
pp. 43-44
Author(s):  
Yuuki OKUZONO ◽  
Fujio AKAGI ◽  
Youichi ANDO ◽  
Masato FURUKAWA ◽  
Sumio YAMAGUCHI
Keyword(s):  
Boundary Layer ◽  
Vortex Ring ◽  
Jet Flow ◽  
Nozzle Wall ◽  
Wall Boundary Layer ◽  
Wall Boundary ◽  
Stable Formation
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