Ongoing Aeroelastic Prediction and Validation Activities at NASA Langley Research Center

[1]  Bret Stanford,et al.  Multiscale Mesh Adaptation for Transonic Aeroelastic Flutter Problems , 2021, AIAA AVIATION 2021 FORUM.

[2]  Bret Stanford,et al.  Aeroelastic Model Development for the Integrated Adaptive Wing Technology Maturation Project Wind-Tunnel Test , 2020 .

[3]  Stephen L. Wood,et al.  Adjoint-based Sensitivities of Flutter Predictions based on the Linearized Frequency-domain Approach , 2020, AIAA Scitech 2021 Forum.

[4]  Marilyn J. Smith,et al.  Evaluation of time-domain damping identification methods for flutter-constrained optimization , 2019, Journal of Fluids and Structures.

[5]  Joaquim R. R. A. Martins,et al.  OpenMDAO: an open-source framework for multidisciplinary design, analysis, and optimization , 2019, Structural and Multidisciplinary Optimization.

[6]  Marilyn J. Smith,et al.  An Aeroelastic Coupling Framework for Time-accurate Analysis and Optimization , 2018 .

[7]  William L. Oberkampf,et al.  Assessment Criteria for Computational Fluid Dynamics Model Validation Experiments , 2017 .

[8]  Qiqi Wang,et al.  CFD-based Aeroelastic Adjoint Sensitivities for Flight Vehicle Weight Minimization Using Sizing and Shape Design Variables , 2017 .

[9]  Bret Stanford,et al.  Uncertainty Quantification of the FUN3D-Predicted Flutter Boundary on the NASA CRM , 2017 .

[10]  Jeffrey A. Housman,et al.  Overset Grid Simulations for the Second AIAA Aeroelastic Prediction Workshop , 2017 .

[11]  Walter A. Silva,et al.  Evaluation of linear, inviscid, viscous, and reduced-order modelling aeroelastic solutions of the AGARD 445.6 wing using root locus analysis , 2014 .

[12]  Carol D. Wieseman,et al.  Overview of the Aeroelastic Prediction Workshop , 2013 .

[13]  Joaquim R. R. A. Martins,et al.  Extensions to the design structure matrix for the description of multidisciplinary design, analysis, and optimization processes , 2012, Structural and Multidisciplinary Optimization.

[14]  R. Walters,et al.  Point-Collocation Nonintrusive Polynomial Chaos Method for Stochastic Computational Fluid Dynamics , 2010 .

[15]  Dimitri J. Mavriplis,et al.  Adjoint-Based Sensitivity Formulation for Fully Coupled Unsteady Aeroelasticity Problems , 2009 .

[16]  Robert W. Moses,et al.  Transport Wing Flutter Model Transonic Limit Cycle Oscillation Test , 2009 .

[17]  Qiqi Wang,et al.  Minimal Repetition Dynamic Checkpointing Algorithm for Unsteady Adjoint Calculation , 2009, SIAM J. Sci. Comput..

[18]  John W. Edwards,et al.  Calculated Viscous and Scale Effects on Transonic Aeroelasticity , 2008 .

[19]  Bruno Sudret,et al.  Global sensitivity analysis using polynomial chaos expansions , 2008, Reliab. Eng. Syst. Saf..

[20]  Dale M. Pitt,et al.  Probabilistic Aeroelastic Analysis and Its Implications on Flutter Margin Requirements , 2008 .

[21]  Chris L. Pettit,et al.  Uncertainty Quantification in Aeroelasticity: Recent Results and Research Challenges , 2004 .

[22]  R. J. Zwaan,et al.  Verification of calculation method for unsteady airloads in the prediction of transonic flutter , 1984 .