Shock tunnel investigation of boundary-layer transition at M equals 5.5

1966 ◽  
Author(s):  
G. RUSHTON
AIAA Journal ◽  
1967 ◽  
Vol 5 (5) ◽  
pp. 899-906 ◽  
Author(s):  
GEORGE H. RUSHTON ◽  
KENNETH F. STETSON

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