A DIFFERENCE METHOD FOR THE SOLUTION OF THE UNSTEADY QUASI-ONE-DIMENSIONAL VISCOUS FLOW IN A DIVERGENT DUCT.
POLYTECHNIC INST OF BROOKLYN FARMINGDALE N Y DEPT OF AEROSPACE ENGINEERING AND APPLIED MECHANICS
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The differential equations describing the unsteady, quasi-one-dimensional flow of a viscous, heat conducting, compressible gas are solved. A time-dependent finite difference scheme is used to integrate the equations. Several features of the shock wave solution are shown and discussed. Author
- Fluid Mechanics