NASA NTRS · 19890000187
Computing Flutter Boundaries
Abstract
MISER2 computer program calculates flutter boundaries and aeroelastic response of cascade of arbitrarily mistuned airfoils. Based on typical section formulation incorporating incompressible, subsonic and supersonic cascade, unsteady aerodynamic theories. Each blade modeled as two-degree-of-freedom oscillator that has inertial coupling between bending and torsional motions. Written in FORTRAN 4.
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Kielb, Robert E., Kaza, Krishna Rao V.. 1989-04-01. Computing Flutter Boundaries. https://ntrs.nasa.gov/citations/19890000187
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