참고문헌 (20)

1. Son, C., Oh, S. and Yee, K., "Ice Accretion on Helicopter Fuselage considering Rotor-wake Effects," Journal of Aircraft, Vol. 54, No. 2, 2017, pp. 500~518. 

   상세보기

2. Son, C. and Yee, K., "Procedure for Determining Operation Limits of High-altitude Long-endurance Aircraft under Icing Conditions," Journal of Aircraft, Vol. 55, No. 1, 2018, pp. 294~309. 

   상세보기

3. Min, S. and Yee, K., "New Roughnessinduced Transition Model for Simulation Ice Accretion on Airfoils," AIAA Journal, Vol. 59, No. 1, 2021, pp. 250~262. 

   상세보기

4. Potapczuk, M. G., "Aircraft Icing Research at NASA Glenn Research Center," Journal of Aerospace Engineering, Vol. 26, No. 2, 2013 pp. 260~276. 

   상세보기

5. Shin, J. and Thomas, B., "Results of an Icing Test on a NACA 0012 Airfoil in the NASA Lewis Icing Research Tunnel," Proceeding of 30th Aerospace Sciences Meeting and Exhibit, 1992. 

6. Bishop, C. M., Pattern Recognition and Machine Learning, Springer, New York, 2006. 

7. Wright, G. B., Radial Basis Function Interpolation: Numerical and Analytical Developments, University of Colorado at Boulder, 2003. 

8. Jeong, S., Murayama, M. and Yamamoto, K., "Efficient Optimization Design Method using Kriging Model," Journal of Aircraft, Vol. 42, No. 2, 2005, pp. 413~420. 

   상세보기

9. Simpson, T. W., Mauery, T. M., Korte, J. J. and Mistree, F., "Kriging Models for Global Approximation in Simulation-based Multidisciplinary Design Optimization," AIAA Journal, Vol. 39, No. 12, 2001, pp. 2233~2241. 

   상세보기

10. Martin, J. D. and Simpson, T. W., "Use of Kriging Models to Approximate Deterministic Computer Models," AIAA Journal, Vol. 43, No. 4, 2005, pp. 853~863. 

    상세보기

11. Sirovich, L., "Turbulence and the Dynamics of Coherent Structures. I. Coherent Structures," Quaterly of Applied Mathmatics," Vol. 45, No. 3, 1987, pp. 561~571. 

12. Guo, M. and Hesthaven, J. S., "Data-driven Reduced Order Modeling for Time-dependent Problems," Computer Methods in Applied Mechanics and Engineering, Vol. 345, 2019, pp. 75~99. 

    상세보기

13. Xiao, D., Yang, P., Fang, F., Xiang, J., Pain, C. C. and Navon, I. M., "Non-intrusive Reduced Order Modelling of Fluid-structure Interactions," Computer Methods in Applied Mechanics and Engineering, Vol. 303, 2016, pp. 35~54. 

    상세보기

14. Audouze, C., De Vuyst, F. and Nair, P. B., "Reduced-Order Modeling of Parameterized PDEs using Time-space-Parameter Principal Component Analysis," International Journal for Numerical Methods in Engineering, Vol. 80, No. 8, 2009, pp. 1025~1057. 

    상세보기

15. Jung, S. K., Shin, S., Myong, R. S. and Cho, T. H., "An Efficient CFD-based Method for Aircraft Icing Simulation using a Reduced Order Model," Journal of Mechanical Science and Technology, Vol. 25, No. 3, 2011, pp. 703~711. 

    원문보기 상세보기

16. Fossati, M. and Habshi W. G., "Multiparameter Analysis of Aero-icing Problems using Proper Orthogonal Decomposition and Multidimensional Interpolation," AIAA Journal, Vol. 51, No. 4, 2013, pp. 946~960. 

    상세보기

17. Zhan, Z., Habashi, W. G. and Fossati, M., "Local Reduced-order Modeling and Iterative Sampling for Parametric Analysis of Aero-icing Problems," AIAA Journal, Vol. 53, No. 8, 2015, pp. 2174~2185. 

    상세보기

18. Zhan, Z., Habashi, W. G. and Fossati, M., "Real-Time Regional Jet Comprehensive Aero-icing Analysis via Reduced-order Modeling," AIAA Journal, Vol. 54, No. 12, 2016, pp. 3787~3802. 

    상세보기

19. Jeck, R. K., "Icing Design Envelops (14 CFR Parts 25 and 29, Appendix C) Converted to a Distance-based Format," Federal Aviation Administration Rept. DOT/FAA/AR-00.30, 2002. 

20. McKay, M. D., Beckman, R. J. and Conover, W. J., "A Comparison of Three Methods for Selecting Values of Input Variables in the Analysis of Output from a Computer Code," Technometrics, Vol. 42, No. 1, 2000, pp. 55~61. 

    상세보기