Authors
Abstract
The Two-dimension ramp inlet flow field was studied with typical mode operations.
Euler equations were used for solution with no special treatment required. In this work a
solution algorithm based on finite difference MacCormack’s technique was developed to
solve mixed subsonic-supersonic flow problem through the external shock diffusers
(ramp inlet) and it is found to be converge for supercritical and critical inlet operation.
Keywords
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