Introduction to Aircraft Aeroelasticity and Loads

By J. Wright, J. Cooper. 2007

676 citations recorded by the source corpus.

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

Design of Composite Wings Including Uncertainties : A Probabilistic Approach (2009, methodology): “Stochastic expansion can be through either the KL [22] or polynomial chaos expansion (PCE).”
Improved aeroelastic tailoring using tow-steered composites (2013, methodology): “In practice, the gust vertical air velocity is assumed to decrease as the gust length decreases [39].”
Reduced order unsteady aerodynamic modeling for stability and control analysis using computational fluid dynamics (2014, background): “2(a) which shows that the unsteady lift increases asymptotically in time to reach the quasisteady value at one degree angle of attack, while it reaches almost 90% of this value after traveling a distance equivalent to 15 semichords [88].”
Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics (2012, methodology): “The DLM underwent further refinements conducted mainly by Rodden and different collaborators [56–59], to become broadly used for unsteady load computations and the prevalent tool in subsonic aircraft aeroelasticity [60].”
Introduction to Nonlinear Aeroelasticity (2017, background): “There exist several good textbooks on linear aeroelasticity for aircraft (Bisplinghoff et al. 1996; Fung 1993; Hodges and Alvin Pierce 2002; Wright and Cooper 2015).”