Numerical investigation of stability of a supersonic laminar boundary layer

1974 ◽  
Vol 13 (5) ◽  
pp. 752-755
Author(s):  
A. A. Maslov
1976 ◽  
Vol 80 (3) ◽  
pp. 541-554 ◽  
Author(s):  
N. Riley

The response of a supersonic laminar boundary layer is considered when fluid is blown obliquely into it from a slot in the boundary. The velocity and length scales associated with the slot blowing are chosen in such a way that the triple-deck theory of Stewartson (9) may be exploited. It is shown that, depending upon the blowing angle, there can be either a compressive or expansive interaction between the boundary layer and free stream upstream from the slot.


AIAA Journal ◽  
1963 ◽  
Vol 1 (1) ◽  
pp. 148-158 ◽  
Author(s):  
STEVEN I. FREEDMAN ◽  
JOHN R. RADBILL ◽  
JOSEPH KAYE

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