Development and Validation of a Fluid–Structure Solver for Transonic Panel Flutter

Author:

Alder Marko1

Affiliation:

1. DLR, German Aerospace Center, 38108 Brunswick, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference33 articles.

1. Historical Development of Aircraft Flutter

2. NicholsJ. “Final Report: Saturn V, S-IVB Panel Flutter Qualification Test,” NASA TN-D-5439, 1969.

3. LallT. “Interstage Adapter Panel Flutter on Atlas-Centaur AC-2, AC-3, and AC-4 Vehicles,” NASA TM-X-1179, 1965.

4. DowellE. H., Aeroelasticity of Plates and Shells, Noordhoff International, Leyden, The Netherlands, 1975, p. 139.

5. Panel flutter - A review of the aeroelastic stability of plates and shells

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