Reduced-Order Modeling of Unsteady Aerodynamics for an Elastic Wing with Control Surfaces-Reference-Cited by-同舟云学术

Reduced-Order Modeling of Unsteady Aerodynamics for an Elastic Wing with Control Surfaces

Published:2017-05 Issue:3 Volume:30 Page:04016083
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Haojie¹,Huang Rui²,Zhao Yonghui³,Hu Haiyan⁴

Affiliation:

1. Ph.D. Student, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, 29 Yudao St., Nanjing 210016, P.R. China.

2. Lecturer, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, 29 Yudao St., Nanjing 210016, P.R. China.

3. Professor, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, 29 Yudao St., Nanjing 210016, P.R. China.

4. Professor, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, 29 Yudao St., Nanjing 210016, P.R. China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000682

Reference29 articles.

1. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.

2. Towards Real-Time Computational-Fluid-Dynamics-Based Aeroelastic Computations Using a Database of Reduced-Order Information

3. Reduced Order Nonlinear System Identification Methodology

4. Transonic aeroelastic simulation for instability searches and uncertainty analysis

5. Application of Multi-Input Volterra Theory to Nonlinear Multi-Degree-of-Freedom Aerodynamic Systems

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