Aeroelastic prediction of the limit cycle oscillations of a cropped delta wing
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering
Reference23 articles.
1. ANSYS, 2002. ANSYS User Manual, Release 7.1. Swanson Analysis Systems, Inc.
2. Attar, P., Dowell, E., Tang, D., 2003a. Modeling aerodynamic nonlinearities for two aeroelastic configurations: delta wing and flapping flag. In: 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, No. 1402.
3. Theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model;Attar;Journal of Fluids and Structures,2003
4. Attar, P., Dowell, E., White, J., 2004a. Modeling the LCO of a delta wing using a high fidelity structural model. Journal of Aircraft 42 (5), 1209–1217.
5. Attar, P., Dowell, E., White, J., 2004b. Modeling the LCO of a delta wing using a high fidelity structural model. AIAA Paper 2004-1402.
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