Design of scaled down models for predicting shell vibration response

Journal of Sound and Vibration

Volumn 195, Issue 2, 1996, Pages 301-311

  Rezaeepazhand, J ^a   Simitses, G J ^a   Starnes Jr , J H ^b  

^a 705 Engineering Research Center   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DYNAMIC RESPONSE; FORECASTING; GEOMETRY; MATHEMATICAL MODELS; SHELLS (STRUCTURES);

SCALED DOWN MODELS; SCALING LAWS; SHELL VIBRATION RESPONSE; SIMILITUDE THEORY;

VIBRATIONS (MECHANICAL);

EID: 0030213041     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1996.0423     Document Type: Article

References (9)

1. A. A. EZRA 1962 NASA TN-D 1510, 661-670. Similitude requirements for scale model determination of shell buckling under impulsive pressure.
2. G. W. MORGEN 1964 AIAA 5th Annual Structures and Materials Conference, Palm Spring, CA, April, 333-343. Scaling techniques for orthotropic cylindrical aerospace structures.
3. W. SOEDEL 1971 Journal of the Acoustical Society of America 49(5), 1535-1541. Similitude approximations for vibrating thin shells.
4. G. J. SIMITSES and J. REZAEEPAZHAND 1993 Journal of Composites Engineering 3(7-8), 751-765. Structural similitude for laminated structures.
5. J. REZAEEPAZHAND, G. J. SIMITSES and J. H. STARNES, JR. 1995 Composite Structures 30, 419-426. Use of scaled-down models for predicting vibration response of laminated plates.
6. J. REZAEEPAZHAND and G. J. SIMITSES 1994 Proceedings of the American Society for Composites, 9th Technical Conference, Newark, DE, 905-912. Scaled down models for stability analysis of laminated cylindrical shells.
7. R. M. JONES 1968 American Institute of Aeronautics and Astronautics Journal 6(12), 2301-2305. Buckling of circular cylindrical shells with multiple orthotropic layers and eccentric stiffeners.
8. R. M. JONES and H. S. MORGAN 1975 American Institute of Aeronautics and Astronautics Journal 13(5), 664-671. Buckling and vibration of cross-ply laminated circular cylindrical shells.
9. S. KELLAS and J. MORTON 1992 American Institute of Aeronautics and Astronautics Journal 30(4), 1074-1080. Strength scaling in fiber composites.