Physics-Based Low-Order Model for Transonic Flutter Prediction

Author:

Opgenoord Max M. J.1,Drela Mark1,Willcox Karen E.1

Affiliation:

1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference53 articles.

1. BradleyM. K.DroneyC. K. “Subsonic Ultra Green Aircraft Research: Phase I Final Report,” Aeronautics and Space Administration (NASA), Boeing Research & Technology, Tech. Rept. NASA/CR2011-216847, National Huntington Beach, CA, April 2011.

2. Towards Gradient-Based Design Optimization of Flexible Transport Aircraft with Flutter Constraints

3. Multidisciplinary Design Optimization of Medium-Range Transonic Truss-Braced Wing Aircraft with Flutter Constraint

4. Review of unsteady transonic aerodynamics: Theory and applications

5. MykytowW. J. “A Brief Overview of Transonic Flutter Problems,” 44th Meeting of the AGARD Structures and Materials Panel, AGARD-CP-226, North Atlantic Treaty Organization, Lisbon, Portugal, 1977, pp. 11-1–11-11.

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