Application of Transonic Codes to Flutter Analysis of Conventional and Supercritical Airfoils
Author:
Affiliation:
1. Purdue University, W. Lafayette, Ind.
2. Informatics, Inc., Palo Alto, Calif.
3. University of Oklahoma, Norman, Okla.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.57378
Reference33 articles.
1. Role of Shocks in the "Sub-Transonic" Flutter Phenomenon
2. Implicit Finite-Difference Computations of Unsteady Transonic Flows about Airfoils
3. Results of an improved version of LTRAN2 for computing unsteady airloads on airfoils oscillating in transonic flow
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