Characteristics method for stress waves from hypervelocity impact of circular cylinder on half space, discussing numerical diffusion effect on pressure and flow fields
Stress waves resulting from hypervelocity impact.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, HYPERVELOCITY IMPACT CONFERENCE ; 1969 ; CINCINNATI, OHIO
1969-04-01
Conference paper
No indication
English
Stress waves resulting from hypervelocity impact
AIAA | 1969
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Engineering Index Backfile | 1965
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