Uncertainty Quantification in Gust Loads Analysis of a Highly Flexible Aircraft Wing

[1]  Hamed Haddad Khodaparast Efficient Worst Case 1-Cosine Gust Loads Prediction , 2012 .

[2]  Thomas Rendall,et al.  57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference , 2016 .

[3]  Jonathan E. Cooper,et al.  Introduction to Aircraft Aeroelasticity and Loads , 2007 .

[4]  Carlos E. S. Cesnik,et al.  Modified Generalized-Alpha Method for Integrating Governing Equations of Very Flexible Aircraft , 2006 .

[5]  Luke A. Lambert,et al.  Aeroelastic Modelling of Highly Flexible Wings , 2016 .

[6]  J. Cooper,et al.  Design of Composite Wings Including Uncertainties : A Probabilistic Approach , 2009 .

[7]  Marty K. Bradley,et al.  Subsonic Ultra Green Aircraft Research , 2011 .

[8]  Carlos E. S. Cesnik,et al.  Finite element solution of nonlinear intrinsic equations for curved composite beams , 1995 .

[9]  D. Hodges A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams , 1990 .

[10]  J. Gordon Leishman,et al.  Unsteady lift of a flapped airfoil by indicial concepts , 1994 .

[11]  Jonathan E. Cooper,et al.  Geometrical Based Method for the Uncertainty Quantification of Correlated Aircraft Loads , 2016 .

[12]  Grégory Coussement,et al.  Uncertainty quantification of simultaneous operational and geometrical uncertainties in turbomachinery design practice , 2015 .

[13]  Jonathan E. Cooper,et al.  Worst Case Gust Prediction of Highly Flexible Wings , 2017 .

[14]  R. Ghanem,et al.  Stochastic Finite Elements: A Spectral Approach , 1990 .

[15]  Timothy J. Allen,et al.  SUGAR Truss Braced Wing Full Scale Aeroelastic Analysis and Dynamically Scaled Wind Tunnel Model Development , 2015 .