Numerical Investigation on the Aeroelastic Instability of a Complete Aircraft Model
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چکیده
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چکیده ندارد.
Identification of a Nonlinear Aeroelastic Aircraft Wing Model
The “reverse path” spectral method, a frequency domain based nonlinear system identification technique, is considered for identifying nonlinear aeroelastic models. The method is based upon a multi-input/multi-output spectral conditioning process that mutually uncorrelates the linear and nonlinear components of the system response. Conditioned frequency response estimates derived from this proce...
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ژورنال
عنوان ژورنال: JSME International Journal Series B
سال: 2005
ISSN: 1340-8054,1347-5371
DOI: 10.1299/jsmeb.48.212