References
- Park, K.H., "Study on the POD Basis Weight Estimation Method for the Reduced Order Model of Aero-Structural Analysis of a Fighter Wing/Fuselage system," Workshop presentation file, The Korean Society For Aeronautical And Space Science, 2012, 1467-1473.
- Kwon, H.J., "Flutter Stability Prediction Using the Unsteady Aerodynamic Reduced-Order Model," Doctoral thesis, Korean Advanced Institute of Science and Technology, 2004.
- McNamara, J. J., Culler, A. J., Crowell, A. R., "Aerothermoelastic Modeling Considerations for Hypersonic Vehicles," 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, 2009.
- Culler, A. J., and McNamara, J. J., "Studies on Fluid-Thermal Structural Coupling for Aerothermoelasticity in Hypersonic Flow," AIAA Journal, Vol. 48, No. 8, Aug. 2010, pp. 1721-1738. https://doi.org/10.2514/1.J050193
- Crowell, A. R., McNamara, J. J., Kecskemety, K. M., and Goerig, T. W., "A Reduced Order Aerothermodynamic Modeling Framework for Hypersonic Aerothermoelasticity," Proceedings of the 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Orlando, Florida.
- Crowell, A. R., McNamara, J. J., "Model Reduction of Computational Aerothermodynamics for Hypersonic Aerothermoelasticity," AIAA Journal, Vol. 50, No. 1., pp. 74-84. https://doi.org/10.2514/1.J051094
- Falkiewicz, N. J., "Reduced-Order Aerothermoelastic Analysis of Hypersonic Vehicle Structures," Ph.D. Dissertation, The University of Michigan, 2012.
- McNamara, J. J., Culler, A. J., Crowell, A. R., "Aerothermoelastic Modeling Considerations for Hypersonic Vehicles," 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, America, 2009.
- Culler, A. J., McNamara, J. J., "Studies on Fluid-Thermal-Structural Coupling for Aerothermoelasticity in Hypersonic Flow," AIAA Journal, Vol. 48, No. 8, Aug. 2010, pp. 1721-1738. https://doi.org/10.2514/1.J050193
- Roe, P.L., "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes," Journal of Computational Physics, Vol. 32, 1981, pp.357-372.
- Van Leer, B., "Towards the ultimate conservative difference scheme. II. Monotonicity and conservation combined in a second-order scheme," Journal of computational physics, Vol.14, No.4, 1974, pp.361-370. https://doi.org/10.1016/0021-9991(74)90019-9
- Lee, N., Lee, S., Cho, H., Kwak, J. Y., Shin, S. J., "Computational analysis for flapping wing by coupled CFD and CSD solutions," 29th Congress of the International Council of the Aeronautical Sciences, St. Petersburg, Russia, 2014.
- Rendall, T. C. S., and Allen, C.B., "Unified fluid-structure interpolation and mesh motion using radial basis functions," International Journal For Numerical Method Engineering., Vol. 74, Issue. 10, 2008, pp. 1519-1559. https://doi.org/10.1002/nme.2219
- Wright, G.B., "Radial basis function interpolation: numerical and analytical developments," Ph.D. Dissertation, The University of Colorado, 2003.
- Zhang, W. W., Ye, Z. Y., Zhang, C. A., "Supersonic Flutter Analysis Based on a Local Piston Theory," AIAA Journal, Vol. 47, No. 10, 2009, pp. 2321-2328. https://doi.org/10.2514/1.37750
- Krige, D.G., "Statistical approach to some basic mine valuation problems on Witwatersrand," Chemical Metallurgical Mining Society, Vol. 53, No.2, 1952, pp.43-44.
- Lophaven, S. N., Nielsen, H. B., and Sondergaard, J., "DACE A Matlab Kriging Toolbox Version 2.0," Technical Report IMMTR-2002-12, Aug., 2002.