A Users Manual for Computer Code Nozzle.
BALLISTIC RESEARCH LABS ABERDEEN PROVING GROUND MD
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A perturbation formula to describe the flow in the transonic region of an axisymmetric nozzle is combined with a computer code which calculates the flow in the supersonic region by the method of characteristics. The perturbation parameter used in the transonic analysis is the normalized radius of curvature of the nozzle throat. Instructions for running the combined code, called NOZZLE, and a tabulation of the output from a test case are included. Authro
- Computer Programming and Software
- Fluid Mechanics