Uncertainty Quantification of the Goland+ Wing's Flutter Boundary
Author:
Affiliation:
1. U.S. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-6309
Reference17 articles.
1. Role of Shocks in the "Sub-Transonic" Flutter Phenomenon
2. Time-marching transonic flutter solutions including angle-of-attack effects
3. 5Bendisken, O. and Kousen, K. “Transonic Flutter Analysis Using the Euler Equations,” AIAA Paper 87-0911-CP.
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