Optimum design via PANDA2 of composite sandwich panels with honeycomb or foam cores

Author:

Bushnell David1,Bushnell David1

Affiliation:

1. Lockheed Martin Palo Alto Research Lab., CA

Publisher

American Institute of Aeronautics and Astronautics

Reference34 articles.

1. Vinson, J. R. "Comparison ofoptimized sandwich panelsof variousconstructions subjected toin-plane loads",ProceedingsofFirstInternationalConference on SandwichConstructions, Stockholm Sweden,pp 23-49, of SANDWICH CONSTRUCTIONS I,edited by K-AOlsson and R.P.Reichard,June 1989

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Difficulties in Optimization of Imperfect Stiffened Cylindrical Shells;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

2. Global optimum design of externally pressurized isogrid stiffened cylindrical shells with added T-rings;International Journal of Non-Linear Mechanics;2002-06

3. Finite Element Modeling of the Buckling Response of Sandwich Panels;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22

4. Modeling of Wrinkling in Sandwich Panels under Compression;Journal of Engineering Mechanics;1999-08

5. Local postbuckling analysis for perfect and imperfect longitudinally compressed plates and panels;39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit;1998-04-20

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