Inviscid Blunt Body Shock Layers (Two-Dimensional Symmetric and Axisymmetric Flows)
POLYTECHNIC INST OF BROOKLYN FARMINGDALE United States
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The results of a time-dependent computation of blunt body shock layers for two-dimensional symmetric and axisymmetric flows are presented in a systematic form for a range of values of the free stream Mach number and bodies of different shapes and variable bluntness. A brief discussion of the relevant features of the computational technique is given. The results are presented in a graphical form the graphs were produced by the computer.
- Fluid Mechanics