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Suspension bridge flutter revisited
Aerodynamic forces employed are obtained in real form from simple tests in wind tunnel on bridge deck section models; aerodynamic force determination is made with instrumentation normally used to monitor amplitude of bending and torsional vibrations, plus calculation scheme based upon theory; wind tunnel method was used on section model of original Tacoma Narrows Bridge; three-dimensional flutter is explained by theory developed; exact role of three-dimensional bridge modes in flutter; relation of section model to full three-dimensional bridge; nonlinear aerodynamic characteristics of bridge section; analytical approach to damping allowing for variation in damping ratio of prototype.
Suspension bridge flutter revisited
Aerodynamic forces employed are obtained in real form from simple tests in wind tunnel on bridge deck section models; aerodynamic force determination is made with instrumentation normally used to monitor amplitude of bending and torsional vibrations, plus calculation scheme based upon theory; wind tunnel method was used on section model of original Tacoma Narrows Bridge; three-dimensional flutter is explained by theory developed; exact role of three-dimensional bridge modes in flutter; relation of section model to full three-dimensional bridge; nonlinear aerodynamic characteristics of bridge section; analytical approach to damping allowing for variation in damping ratio of prototype.
Suspension bridge flutter revisited
ASCE Structural Eng Conference -- Prepr
Scanlan, R.H. (author) / Sabzevari, A. (author)
ASCE Structural Engineering Conference ; 1967
1967
35 pages
Conference paper
English
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