scholarly journals Experimental investigation of a two-dimensional shock-turbulent boundary layer interaction with bleed

1983 ◽  
Author(s):  
W. HINGST ◽  
F. TANJI
Keyword(s):  
Boundary Layer ◽  
Experimental Investigation ◽  
Turbulent Boundary Layer ◽  
Two Dimensional ◽  
Layer Interaction ◽  
Boundary Layer Interaction

Effect of Shock Boundary Layer Interaction on Aerofoil Pressure Distributions at Transonic Speeds

1963 ◽  
Vol 67 (634) ◽  
pp. 674-677
Author(s):  
D. Tirumalesa
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Turbulent Boundary Layer ◽  
Two Dimensional ◽  
Relative Thickness ◽  
Circular Arc ◽  
Layer Interaction ◽  
Pressure Distributions ◽  
Boundary Layer Interaction ◽  
Theoretical Results

SummaryA method of improving pressure distributions predicted by inviscid theory over two-dimensional aerofoils at transonic speeds taking into account shock-wave turbulent boundary layer interaction as obtained in the case of the flat plate is described.The method was applied to a non-lifting circular arc aerofoil of eight per cent relative thickness. The shock wave location, pressure distribution and drag coefficient were calculated and compared with experimental and inviscid theoretical results.It has been found that the method gives results which are consistent with experimental results in various aspects.

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