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
01.04.1969
Aufsatz (Konferenz)
Keine Angabe
Englisch
Stress waves resulting from hypervelocity impact
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