NASA NTRS · 19710041383
Analysis of nonlinear panel flutter and response under random excitation or nonlinear aerodynamic loading
Abstract
Nonlinear panel flutter analysis and response under random excitation or nonlinear aerodynamic loading, using Rayleigh-Ritz approximation to Hamilton variational principle
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Eastep, F. E., Mcintosh, S. C., Jr.. 1971-03-01. Analysis of nonlinear panel flutter and response under random excitation or nonlinear aerodynamic loading. https://ntrs.nasa.gov/citations/19710041383
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