Abstract: | This paper presents solutions of subsonic and transonic flow fields in two-dimensional De Laval nozzles with preassinged contraction
ration
1, expansion ration
2, and throat wall radiusR
*. The effects of the contraction and the expansion angle on nozzle flow, the transformation of flow pattern of a De Laval
nozzle in the throat region, and the conditions of occurrence and the governing parameters of the supersonic bubbles are discussed. |