Airframe Stress Analysis and Sizing

By M. Niu. 2011

193 citations recorded by the source corpus.

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Design, Optimization, and Evaluation of Integrally Stiffened Al-7050 Panel with Curved Stiffeners (2011, background): “(4), is obtained from page 444 of [6].”
Fail-safe topology optimization (2016, methodology): “Fail-safe requirement for aircraft design was clearly defined in two books by Niu that are widely used handbooks by aerospace structural engineers—‘Aircraft structural design’ and ‘Airframe structural analysis and sizing’ (Niu 1988, 1997).”
Coupled adjoint aerostructural wing optimization using quasi-three-dimensional aerodynamic analysis (2015, methodology): “The upper and lower equivalent panels are in fact stiffened panels, therefore the stiffened panel efficiency method (Niu 1997) is used to compute the buckling load for those panels.”