Geometrically exact finite element for thin shells of revolution, using approximation to predict boundary layer stress distribution during vibration
A geometrically exact finite element for thin shells of revolution.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING ; 1969 ; NEW YORK, NY
01.01.1969
Aufsatz (Konferenz)
Keine Angabe
Englisch
Finite element solution for thin shells of revolution
TIBKAT | 1964
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