Gradient Based Optimization using Spectral Formulation-Based FSI and Coupled Sensitivity Analysis

Author:

Prasad Rachit1,Yi Seulgi2,Choi Seongim1,Im Dongkyun1

Affiliation:

1. Virginia Polytechnic Institute and State University

2. Korea Advanced Institute of Science and Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference37 articles.

1. Physical mechanisms for limit-cycle oscillations of a cropped delta wing

2. Comparison of finite volume flux vector splittings for the Euler equations

3. Two efficient staggered algorithms for the serial and parallel solution of three-dimensional nonlinear transient aeroelastic problems

4. 4Bae, J. "Aeroelastic characteristics and flutter suppression considering structural nonlinearity", Ph.D Dissertation,Korea Advanced Institute of Science and Technology, Republicof Korea,2002.

5. 5Kim, J. "Transonic aeroelastic analysis of wings with aerodynamic nonlinearities", Ph.D Dissertation,Korea Advanced Institute of Science and Technology, Republicof Korea,2008.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Analysis and Sensitivity Calculation using High Fidelity Spectral Formulation-Based FSI and Coupled Adjoint Method;17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2016-06-10

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