1 |
Wempner, G. A. and Wilms, E.V., Multi-rail launcher with six degrees of freedom, University of Alabama Research Institute, 1966.
|
2 |
Przemieniecki, J.S., "Matrix structural analysis of substructures", AIAA Journal, Vol. 1, No.1, 1963, pp.138-147.
DOI
|
3 |
Hurty,W.C., "Dynamic analysis of structural systems using component modes", AIAA Journal, Vol. 3, No.4, 1965, pp. 678-685.
DOI
|
4 |
Craig, R.R. and Bampton, M.C.C., "Coupling of substructures for dynamic analysis" AIAA Journal, Vol.6, No.7, 1968, pp.1313-1319.
DOI
|
5 |
Grimes, P.J., McTigue, L.D., Riley, G.F. and Tilden, D.I., Advancements in structural dynamic technology resulting from Saturn V programs, NASA CR-1539, June 1970.
|
6 |
Benfield, W.A. and Hruda, R.F. "Vibration analysis of structures by component mode substitution", AIAA Journal, Vol. 9, No.7, 1971, pp.1255-1261.
DOI
|
7 |
Goldenberg, S. and Shapiro, M., A study of modal coupling procedures for the space shuttle, NASACR-112252, 1973.
|
8 |
Agrawal, B.N., "Mode synthesis technique for dynamic analysis of structures", The Journal of the Acoustical Society of America, Vol.59, 1976, pp.1329-1338. DOI:10.1121/1.381019.
DOI
ScienceOn
|
9 |
Thornton, E.A., Vibration analysis of a 1/15 scale dynamic model of a space shuttle configuration, NASA CR-111984, 1971.
|
10 |
Urgueira, A.P.V., Dynamic analysis of coupled structures using experimental data, University of London, 1989.
|
11 |
Friswell, M. and Mottershead, J.E., Finite Element Model Updating in Structural Dynamics, Kluwer Academic Publishers, 1996.
|
12 |
Buehrle, R.D., Fleming, G.A. and Pappa, R.S., "Finite element model development and validation for aircraft fuselage structures". 18th International Modal Analysis Conference, San Antonio, Texas, 2000.
|
13 |
Hu, H., Wang, Y. and Lu, W., "Structural dynamic analysis of a sounding rocket during the liftoff", Journal of Aeronautics, Astronautics ans Aviation, Vol.41, No.2, 2009, pp.111-120.
|
14 |
De Vivo, A., Brutti, C. and Leofanti, J.L., "Modal shape identification of large structure exposed towind excitation by operational modal analysis technique", Mechanical Systems and Signal Processing, Vol.39, 2013, pp.195-206.
DOI
|
15 |
Fransen, S., Rixen, D., Henricksen, T. and Bonnet, M., "On the operational modal analysis of solid rocket motors", In: Proceedings of the 28th International Modal Analysis Conference, Jacksonville, Florida, USA, February 1-4, 2010.
|
16 |
Isik, S.K., Ider, C. and Acar, B., "Modeling and verification of a missile launcher system", Journal of Multibody Dynamics, Vol. 228, 2014, pp. 100-107.
|
17 |
Carrera, E., "A class of two dimensional theories for multilayered plates analysis". Atti Accademia delle Scienze di Torino, Memorie Scienze Fisiche, Vol. 19-20, 1995, pp. 49-87.
|
18 |
Carrera, E., "Theories and finite elements for multilayered, anisotropic, composite plates and shells", Archives of Computational Methods in Engineering, Vol.9, No. 2, 2002, pp.87-140.
DOI
|
19 |
Carrera, E., "Theories and finite elements for multilayered plates and shells: a unified compact formulation with numerical assessment and benchmarking", Archives of Computational Methods in Engineering, Vol.10, No.3, 2003, pp. 216-296.
|
20 |
Carrera, E. and Giunta, G., "Refined beam theories based on a unified formulation", International Journal of Applied Mechanics, Vol. 2, No. 1, 2010, pp.117-143.
DOI
|
21 |
Carrera, E., Pagani, A. and Petrolo, M., "Classical, refined and component-wise analysis of reinforced-shell structures", AIAA Journal, Vol. 51, No. 5, 2013, pp. 1255-1268.
DOI
|
22 |
Carrera, E., Giunta, G., Nali, P. and Petrolo, M., "Refined beam elements with arbitrary cross-section geometries", Computers & Structures, Vol.88. No.5-6, 2010, pp.283-293.
DOI
ScienceOn
|
23 |
Carrera, E., Petrolo, M. and Zappino, E., "Performance of CUF approach to analyze the structural behavior of slender bodies", Journal of Structural Engineering, Vol.138, No. 2, 2012, pp. 285-297. DOI:10.1061/(ASCE)ST.1943-541X.0000402.
DOI
|
24 |
Carrera, E., Petrolo, M. and Nali, P., "Unified formulation applied to free vibrations finite element analysis of beams with arbitrary section", Shock and Vibrations, Vol. 18, No. 3, 2011, pp. 485-502.
DOI
|
25 |
Carrera, E., Pagani, A. and Petrolo, M., "Componentwise method applied to vibration of wing structures", Journal of Applied Mechanics, Vol. 88, No. 4, 2013, pp. 041012.1-041012.15.
|
26 |
Carrera, E., Pagani, A. and Petrolo, M., "Classical, refined, and component-wise analysis of reinforced-shell wing structures". AIAA Journal, Vol. 51, No. 5, 2013, pp. 1255-1268. DOI:10.2514/1.J052331.
DOI
|
27 |
Carrera, E., Gaetano, G. and Petrolo M., Beam Structures, Classical and Advanced Theories, John Wiley & Sons, 2011.
|
28 |
Carrera, E., Cinefra, M., Petrolo, M. and Zappino, E., Finite Element Analysis of Structures Through Unified Formulation, John Wiley & Sons, 2014.
|