CORSS Cylinder Optimization of Rings Skin and Stringers

CORSS  Cylinder Optimization of Rings  Skin  and Stringers
Author: J. Finckenor
Publsiher: Unknown
Total Pages: 96
Release: 1994
Genre: Electronic Book
ISBN: NASA:31769000447766

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CORSSTOL Cylinder Optimization of Rings Skin and Stringers with Tolerance Sensitivity

CORSSTOL  Cylinder Optimization of Rings  Skin  and Stringers with Tolerance Sensitivity
Author: J. Finckenor
Publsiher: Unknown
Total Pages: 44
Release: 1995
Genre: Mathematical optimization
ISBN: NASA:31769000448566

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Panel Optimization with Integrated Software POIS PANDA

Panel Optimization with Integrated Software  POIS    PANDA
Author: Anonim
Publsiher: Unknown
Total Pages: 266
Release: 1981
Genre: Aircraft
ISBN: MINN:31951D03698573S

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An analysis and an interactive computer program are described through which minimum weight designs of composite, stiffened, cylindrical panels can be obtained subject to general and local buckling constraints and stress and strain constraints. The panels are subjected to arbitrary combinations of in-plane axial, circumferential, and shear resultants. Nonlinear material effects are included if the material is isotropic or has stiffness in only one direction (as does a discrete or a smeared stiffener). Several types of general and local buckling modes are included as constraints in the optimization process, including general instability, panel instability with either stringers or rings smeared out, local skin buckling, local crippling of stiffener segments, and general, panel, and local skin buckling including the effects of stiffener rolling. Certain stiffener rolling modes in which the panel skin does not deform but the cross section of the stiffener does deform are also accounted for. The interactive PANDA system consists of three independently executed modules that share the same data base. In the first module an initial design concept with rough (not necessarily feasible or accurate) dimensions are provided by the user in a conversational mode. In the second module the user decides which of the design parameters of the concept are to be treated by PANDA as decision variables in the optimization phase. In the third module the optimization calculations are carried out. Many examples are provided in which optimum designs obtained by PANDA are compared to those in the literature. (Author).

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author: Anonim
Publsiher: Unknown
Total Pages: 704
Release: 1995
Genre: Aeronautics
ISBN: UIUC:30112050127304

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Monthly Catalogue United States Public Documents

Monthly Catalogue  United States Public Documents
Author: Anonim
Publsiher: Unknown
Total Pages: 752
Release: 1994
Genre: Government publications
ISBN: UIUC:30112005601734

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications
Author: Anonim
Publsiher: Unknown
Total Pages: 135
Release: 1994
Genre: Government publications
ISBN: WISC:89117117382

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Structural Design Concepts

Structural Design Concepts
Author: Louis Albert Scipio
Publsiher: Unknown
Total Pages: 186
Release: 1967
Genre: Building materials
ISBN: UIUC:30112008385996

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Panel Optimization with Integrated Software POIS

Panel Optimization with Integrated Software  POIS
Author: David Bushnell
Publsiher: Unknown
Total Pages: 262
Release: 1981
Genre: Buckling (Mechanics)
ISBN: UOM:39015095307222

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An analysis and an interactive computer program are described through which minimum weight designs of composite, stiffened, cylindrical panels can be obtained subject to general and local buckling constraints and stress and strain constraints. The panels are subjected to arbitrary combinations of in-plane axial, circumferential, and shear resultants. Nonlinear material effects are included if the material is isotropic or has stiffness in only one direction (as does a discrete or a smeared stiffener). Several types of general and local buckling modes are included as constraints in the optimization process, including general instability, panel instability with either stringers or rings smeared out, local skin buckling, local crippling of stiffener segments, and general, panel, and local skin buckling including the effects of stiffener rolling. Certain stiffener rolling modes in which the panel skin does not deform but the cross section of the stiffener does deform are also accounted for. The interactive PANDA system consists of three independently executed modules that share the same data base. In the first module an initial design concept with rough (not necessarily feasible or accurate) dimensions are provided by the user in a conversational mode. In the second module the user decides which of the design parameters of the concept are to be treated by PANDA as decision variables in the optimization phase. In the third module the optimization calculations are carried out. Many examples are provided in which optimum designs obtained by PANDA are compared to those in the literature. (Author)