Recent enhancements to PANDA2
Author:
Affiliation:
1. Lockheed Martin Palo Alto Research Lab., CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1337
Reference59 articles.
1. Optimum design of composite stiffened panels under combined loading
2. Minimum-weight design of a stiffened panel via PANDA2 and evaluation of the optimized panel via STAGS
3. Optimization of composite, stiffened, imperfect panels under combined loads for service in the postbuckling regime
4. Truss-core sandwich design via PANDA2
Cited by 8 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. A Shortened Version of the Report on Minimum Weight Design of Imperfect Isogrid-Stiffened Ellipsoidal Shells Under Uniform External Pressure;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04
2. 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
3. Global optimum design of externally pressurized isogrid stiffened cylindrical shells with added T-rings;International Journal of Non-Linear Mechanics;2002-06
4. Optimization of Perfect and Imperfect Ring and Stringer Stiffened Cylindrical Shells with PANDA2 and Evaluation of the Optimum Designs with STAGS;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22
5. Optimal design of grid-stiffened panels and shells with variable curvature;Composite Structures;2001-05
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