1 |
Kim, B. G., Chung, T. J. and Lee, J. K., 2000, A Study on the Improvement of Finite Element Model for Scaled Frame by Considering Eigenvectors and Eigenvalues, Transactions of the Korean Society for Noise and Vibration Engineering, Vol. 10, No. 6, pp. 1009-1016.
|
2 |
Haimanote, T, K, 2007, Updating of Finite Element Analyticla Model Using Modal Test Results, Department of Mechanical Engineering Addis Ababa University.
|
3 |
Szkudlarek, W., Mizutani, A., Peeters, B., Luczak, M. and Kahsin, M., 2009, Ground Vibration Testing, Finite Element Modeling, and Correlation of a Composite Hobby Aircraft, 13th International Conference on AEROSPACE SCIENCES & AVIATION TECHNOLOGY.
|
4 |
Buehrle, R. D., Fleming, G. A., Pappa, R. S. and Grosveld, F. W., 2000, Finite Element Model Development and Validation for Aircraft Fuselage Structures, 18th International Modal Analysis Conference.
|
5 |
Peeters, B., Climent, H., Raul de Diego., Jesus de Alba., 2008, Modern Solutions for Ground Vibration Testing of Large Aircraft, IMAC 26 USA.
|
6 |
Dorin LOZICI-BRINZEI., Simion TAATARU., Radu BISCAA., 2011, IAR-99 GVT Correlation for Dynamics Stores FEM, INCAS BULLETIN, Vol. 3, Issue 1, pp. 47-54.
DOI
|
7 |
Pickrel, C. R., 2002, Airplane Ground Vibration Testing-nominal Modal Model Correlation, 20th International Modal Analysis Conference, Los Angeles, CA.
|
8 |
Kenneth, G. M., 1995, Vibration Testing, John Wiley & Sons, Inc., New York.
|
9 |
MSC/PATRAN, NASTRAN, 2010.
|
10 |
LMS Virtual. Lab Solutions Guide, LMS Intl., Leuven, 2006.
|