On the use of the P-TFE method for panel flutter optimization

Computers and Structures

Volumn 70, Issue 1, 1999, Pages 109-117

  Barboni, R ^a   Mannini, A ^a   Gaudenzi, P ^a  

^a SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

P TFE method; Panel flutter optimization; Structural analysis

Indexed keywords

BOUNDARY CONDITIONS; EIGENVALUES AND EIGENFUNCTIONS; FLUTTER (AERODYNAMICS); NONLINEAR EQUATIONS; OPTIMIZATION; SENSITIVITY ANALYSIS; STRUCTURAL ANALYSIS;

PANEL FLUTTER OPTIMIZATION;

STRUCTURAL PANELS;

EID: 0032711639     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7949(98)00180-1     Document Type: Article

References (11)

1. Barboni R, Castellani A, Mannini A. Un metodo analitico-numerico per l'analisi strutturale, Atti del Dipartimento Aerospaziale. Roma, Novembre 1988.
2. Barboni R, Gaudenzi P, Mannini A, Santini P. An application to the dynamics of large space structures of a new semi-analytic method for structural analysis, 17th Congress ICAS. Stockholm, September 1990.
3. Barboni R, Gaudenzi P, Mannini A. Parameter-transfer finite element method for structural analysis. AIAA Journal 1993;31:923-9.
4. Barboni R, Mannini A, Scarponi C. Structural optimization with parameter-transfer finite element. Meccanica 1995;30:291-304.
5. Dobbs MW, Nelson RS. Application of optimality criteria to automated structural design. AIAA Journal 1976;14:1436-43.
6. Kjusalaas J, Shaw RCJ. An algorithm for optimal structural design with frequencies constraints. International Journal for Numerical Methods in Engineering 1978;13.
7. Barboni R, Carlini O, Santini P. Ottimizzazione strutturale in campo dinamico, L'Aerotecnica Missili e Spazio. Giugno, 1981.
8. Santini P, Balis Crema L, Peroni I. Structural optimization in aeroelastic conditions. L'Aerotecnica Missili e Spazio, 1976; 1-2.
9. Turner MJ. Optimization of structures to satisfy flutter requirements. AIAA Journal 1969;7(5):945-51.
10. Weisshaar TA. Aeroelastic optimization for a panel in high Mach number supersonic flow. Journal of Aircraft 1972;9(9):611-7.
11. Van Keuren GM, Jr, Eastep FE. Use of Galerkin method for minimum-weight panels with dynamic constraints. Journal of Spacecraft 1977;14(7):414-8.