Index of /turbdata/agard/chapter6/SHL01

	Name	Last modified	Size	Description
	Parent Directory		-
	C01.dat	2011-06-20 13:45	19K
	C02.dat	2011-06-20 13:45	8.3K
	C03.dat	2011-06-20 13:45	19K
	C04.dat	2011-06-20 13:45	16K
	C05.dat	2011-06-20 13:45	1.0K
	C06.dat	2011-06-20 13:45	3.4K

              SHL01 Two stream subsonic mixing layer



**** DATA PUBLISHED IN JOURNAL ARTICLE --- Development of Two-Stream ****
**** Mixing Layer from Tripped and Untripped Boundary Layers ****
**** AIAA JNL. vol.28, 1990) by J.H. Bell and R.D. Mehta ****
Spanwise Averaged Data



........................................................................

1) UNTRIPPED case (laminar boundary layers)

a) Mean velocity U, u', v', w' for 8 streamwise stations:      File C01
Station 0A = 7.8 cm; 2 = 16.7 cm; 3 = 57.3 cm; 4 = 77.6 cm;
4A = 108.1 cm; 5 = 128.4 cm; 6 = 189.4 cm; 7A = 250.3 cm.
N.B.
The error function is provided after the mean velocity data.
(Fig. 2a, 4a-b-c)

b) Turbulent shear stress u'v' and Ruv correlation for
 the same 8 stations:                                          File C02
(Fig. 4d,f)
........................................................................

2) TRIPPED case (turbulent boundary layers)

a) Mean velocity U, u', v', w' for 8 streamwise stations:      File C03
Station 0A = 7.8 cm; 2 = 16.7 cm; 3 = 57.3 cm; 4 = 77.6 cm;
4A = 108.1 cm; 5 = 128.4 cm; 6 = 189.4 cm; 7A = 250.3 cm.
N.B.
The error function is provided after the mean velocity data.
(Fig. 2a, 4a-b-c)


b) Turbulent shear stress u'v' and Ruv correlation for
 the same 8 stations:                                          File C04
(Fig. 4d,f) 
........................................................................

3) Streamwise mixing layer growth: untripped  and tripped:      File C05 
(Fig. 3)

........................................................................

4) Streamwise development of  maximum primary turbulent
stresses: u'v', u', v' and w', untripped  and tripped:          File C06 
(Fig. 5 d,a,b,c)