Transonic flutter analysis of an AGARD 445.6 wing in the frequency domain using the Euler method

References

• Albano, E., & Rodden, W. P. (1969). A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows. AIAA Journal, 7, 279–285. 10.2514/3.5086
   Google Scholar
• Fairuz, Z. M., Abdullah, M. Z., Yusoff, H., & Abdullah, M. K. (2013). Fluid structure interaction of unsteady aerodynamics of flapping wing at low reynolds number. Engineering Applications of Computational Fluid Mechanics, 7(1), 144–158. doi:10.1080/19942060.2013.11015460
   Google Scholar
• Farhangnia, M., Guruswamy, G. P., & Biringen, S. (1996, January). Transonic-buffet associated aeroelasticity of a supercritical wing. Paper presented at the meeting of AIAA 34th Aerospace Sciences Meeting and Exhibit, Reno, NV.
   Google Scholar
• Foerster, M., & Breitsamter C. (2013, June). Computational aeroelastic analysis in time and frequency domain using non-linear and linearized Euler/Navier-Stokes methods. Paper presented at the meeting of International Forum on Aeroelasticity & Structural Dynamics, Bristol, UK.
   Google Scholar
• Gao, C., Luo, S., Liu, F., & Schuster, D. M. (2005). Calculation of airfoil flutter by an Euler method with approximate boundary conditions. AIAA Journal, 43, 295–305. 10.2514/1.5752
   Google Scholar
• Gordnier, R. E., & Melville, R. B. (2001). Numerical simulation of limit-cycle oscillations of a cropped delta wing using the full Navier-Stokes equations. International Journal of Computational Fluid Dynamics, 14, 211–224. 10.1080/10618560108940725
   Google Scholar
• Iovnovich, M., & Raveh, D. E. (2012). Reynolds-averaged Navier-Stokes study of the shock-buffet instability mechanism. AIAA Journal, 50, 880–890. 10.2514/1.J051329
   Google Scholar
• Kreiselmaier, E., & Laschka, B. (2000). Small disturbance Euler equations: Efficient and accurate tool for unsteady load prediction. Journal of Aircraft, 37, 770–778. 10.2514/2.2699
   Google Scholar
• Lee-Rausch, E., & Batina, J. T. (1996). Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations. Journal of Aircraft, 33, 1139–1147. 10.2514/3.47068
   Google Scholar
• Li, D., & Lu, Q. H. (2004). Analysis of experiments in engineering vibration. Beijng: Tsinghua University Press.
   Google Scholar
• Liu, F., Cai, J., Zhu, Y., Tsai, H. M., & Wong, A. S. F. (2001). Calculation of wing flutter by a coupled fluid-structure method. Journal of Aircraft, 38, 334–342. doi:10.2514/2.2766
   Google Scholar
• Obayashi, S., & Guruswamy, G. P. (1995). Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations. AIAA Journal, 33, 1134–1141. doi:10.2514/3.12533
   Google Scholar
• Rodden, W. P., & Johnson, E. H. (1994). MSC/NASTRAN aeroelastic analysis: User's guide (Version 68). Los Angeles, CA: MacNeal-Schwendler Corporation.
   Google Scholar
• Sadeghi, M., Yang, S., Liu, F., & Tsai, H. M. (2003, January). Parallel computation of wing flutter with a coupled Navier-Stokes/CSD method. Paper presented at the meeting of 41st Aerospace Sciences Meeting and Exhibit, Reno, NV.
   Google Scholar
• Wang, G., Mian, H. H., Shan, X., & Lee, J. (2015). Static aeroelastic predictions for complex aircraft configurations with CFD/CSD coupling methodology. AIAA Journal, 7, 279–285. doi:10.2514/6.2015-0253
   Google Scholar
• Yates E. C. (1987). AGARD Standard Aeroelastic Configurations for Dynamic Response candidate configuration I-Wing 445.6. NASA TM-100492.
   Google Scholar
• Zeng, X., Xu, M., An, X., & Chen, S. (2008). Wing flutter analysis using CFD/CSD algorithm. Journal of Northwestern Polytechnical University, 26 (1), 79–82. 10.3969/j.issn.1000-2758.2008.01.016
   Google Scholar
• Zhang, W. (2006). Efficient analysis for aeroelasticity based on computational fluid dynamics (Doctoral dissertation). Retrieved from China Doctoral Dissertations Full-text Database. doi:10.7666/d.y1189904
   Google Scholar
• Zhang, W., Jiang, Y., & Ye, Z. (2007). Two better loosely coupled solution algorithms of CFD based aeroelastic simulation. Engineering Applications of Computational Fluid Mechanics, 1, 253–262. doi:10.1080/19942060.2007.11015197
   Google Scholar
• Zhang, Z., Liu, F., & Schuster, D. M. (2004, August). Calculations of unsteady flow and flutter by an euler and integral boundary-layer method on Cartesian grids. Paper presented at the meeting of 22nd Applied Aerodynamics Conference and Exhibit, Providence, Rhode Island.
   Google Scholar
• Zhang, Z., Yang, S., & Chen, P. C. (2012). Linearized Euler solver for rapid frequency-domain aeroelastic analysis. Journal of Aircraft, 49, 922–932. doi:10.2514/6.2011-3364
   Google Scholar
• ZONA Technology. (2011). ZAERO theoretical manual. Scottsdale, AZ: ZONA Technology.
   Google Scholar