Influence of Shock-Wave Attenuation by Boundary-Layer Growth on Contact-Surface Motion in a Shock Tube

1959 ◽  
Vol 26 (6) ◽  
pp. 388-389 ◽  
Author(s):  
Jan Rosciszewski
1968 ◽  
Vol 18 (1) ◽  
pp. 116-155 ◽  
Author(s):  
P. J. Musgrove ◽  
J. P. Appleton

1947 ◽  
Vol 14 (3) ◽  
pp. A213-A216
Author(s):  
R. C. Binder

Abstract A method is presented for calculating the efficiency of a diffuser for two-dimensional, steady, incompressible flow without separation. The method involves a combination of organized boundary-layer data and frictionless potential-flow relations. The potential velocity and pressure are found after the boundary-layer growth is determined by a trial-and-check calculation.


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