Computational Assessment of Transonic Airfoil-Gust Aeroelastic Response

Author:

Halder Rahul1,Damodaran Murali1,Cheong Khoo Boo1

Affiliation:

1. National University of Singapore, Singapore 117575, Singapore

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference26 articles.

1. Hopf-Bifurcation Analysis of Airfoil Flutter at Transonic Speeds

2. LanchesterF. “Torsional Vibrations of the Tail of an Aeroplane,” Aircraft Research Council R&M 276 (Part 1), 1916.

3. FrazerR.DuncanW. “The Flutter of Aeroplane Wings,” Aeronautical Research Council R&M 1155, 1928. 10.1017/S0368393100132614

4. TheodorsenT. “General Theory of Aerodynamic Instability and the Mechanism of Flutter,” NACA Rept. 496, May 1934.

5. ChenP.LiuD. “A Harmonic Gradient Method for Unsteady Supersonic Flow Calculations,” Journal of Aircraft, Vol. 22, No. 5, May 1985, pp. 371–379. 10.2514/3.45134

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