Publication Date:
2016-06-07
Description:
The inviscid, internal, and external axial corner flows generated by two intersecting wedges traveling supersonically are obtained by use of a second-order shock-capturing, finite-difference approach. The governing equations are solved iteratively in conical coordinates to yield the complicated wave structure of the internal corner and the simple peripheral shock of the external corner. The numerical results for the internal flows compare favorably with existing experimental data.
Keywords:
AERODYNAMICS
Type:
Aerodynamic Analyses Requiring Advanced Computers, Pt. 1; p 643-658
Format:
application/pdf
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