NASA NTRS · 19700038115
Application of aeroelastic constraints in structural optimization
Abstract
Aircraft structural weight optimization for given fundamental vibration frequency obtained by applying aeroelastic constraints, using analytical approach
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Ashley, H., Mcintosh, S. C., Jr.. 1969-01-01. Application of aeroelastic constraints in structural optimization. https://ntrs.nasa.gov/citations/19700038115
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