A Computer Program To Calculate In Plane And Flexural Properties Of Symmetric Laminates On The Hp 87 Microcomputer

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Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1983

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with Aeronautics categories.

A Computer Program To Calculate In Plane And Flexural Properties Of Symmetric Laminates On The Hp 87 Microcomputer

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Author :
language : en
Publisher:
Release Date : 1982

A Computer Program To Calculate In Plane And Flexural Properties Of Symmetric Laminates On The Hp 87 Microcomputer written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with categories.

The computation of parameters for symmetric laminates involves series of tedious calculations for both in-plane and flexural properties. In order to alleviate the magnitude and complexity of calculations for complicated symmetric laminates, the program of this report was designed for a commercially available microcomputer, the Hewlett-Packard HP-87, and is based for the most part on program logic developed by the Air Force Wright Aeronautical Laboratories for the TI-59 handheld programmable calculator. Program logic is explained in detail with flowcharts and a full listing of the program is included. A description of the program logic provides the user with a comprehensive explanation of program operation. (Author).

A Computer Program To Calculate In Plane And Flexural Properties Of Symmetric Laminates On The Hp 87 Microcomputer

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Author : Dennis R. Ferrell
language : en
Publisher:
Release Date : 1982

A Computer Program To Calculate In Plane And Flexural Properties Of Symmetric Laminates On The Hp 87 Microcomputer written by Dennis R. Ferrell and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with categories.

The computation of parameters for symmetric laminates involves series of tedious calculations for both in-plane and flexural properties. In order to alleviate the magnitude and complexity of calculations for complicated symmetric laminates, the program of this report was designed for a commercially available microcomputer, the Hewlett-Packard HP-87, and is based for the most part on program logic developed by the Air Force Wright Aeronautical Laboratories for the TI-59 handheld programmable calculator. Program logic is explained in detail with flowcharts and a full listing of the program is included. A description of the program logic provides the user with a comprehensive explanation of program operation. (Author).

Government Reports Announcements Index

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Author :
language : en
Publisher:
Release Date : 1983

Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with Science categories.

Government Reports Annual Index

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Author :
language : en
Publisher:
Release Date : 1983

Government Reports Annual Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with Government reports announcements & index categories.

Interference Problems On Wing Fuselage Combinations In Inviscid Incompressible Flow

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Author : Aeronautical Research Council (Great Britain)
language : en
Publisher:
Release Date : 1974

Interference Problems On Wing Fuselage Combinations In Inviscid Incompressible Flow written by Aeronautical Research Council (Great Britain) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Airplanes categories.

Government Reports Annual Index Keyword A L

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Author :
language : en
Publisher:
Release Date : 1983

Government Reports Annual Index Keyword A L written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with Government reports announcements & index categories.

Sharp Pc 1500 Pocket Computer Solutions To Composite Materials Formulas

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Author : Won J. Park
language : en
Publisher:
Release Date : 1982

Sharp Pc 1500 Pocket Computer Solutions To Composite Materials Formulas written by Won J. Park and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Laminated materials categories.

This volume contains the description and instructions of the use of Sharp PC-1500 Pocket Computer for the key calculations of the stiffness and strength of symmetric laminated composites. Instant calculations can be made for practical use. The formulas and equation numbers used in the performed programming have been derived from a book entitled, Introduction to Composite Materials, co-authored by S.W. Tsai and H.T. Hahn, published by Technomic Publishing Company, Westport, CT, July 1980. (Author).

Composite Laminate Weight Optimization On The Timex Sinclair 1000 Microcomputer

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Author : Gerald V. Flanagan
language : en
Publisher:
Release Date : 1983

Composite Laminate Weight Optimization On The Timex Sinclair 1000 Microcomputer written by Gerald V. Flanagan and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with categories.

CLASS (Composite Laminate Automated Sizing for Strength) is an interactive optimization program designed to run on a small microcomputer. The listing presented here is for a Sinclair ZX81 or a Timex-Sinclair 1000 microcomputer with a 16K memory expansion. The version of Basic is standard enough that translations to other microcomputers is possible. The program will find a minimum thickness laminate which will not fail under any of the load conditions entered. Ply orientation are chosen by the user. The program's capability in handling multiple, independent, loads could be useful for loads which change with time or for situations where there is uncertainty in calculating the loads. As the program is currently dimensioned, four independent load combinations and 18-ply orientations can be entered. Only point stresses are considered, thus the program optimizes the laminate only at one point in the structure. Furthermore, the program assumes in-plane loads only and no out-of-plane deflections. This implies a symmetric laminate, but stacking sequence is not a factor in the program. The layer thicknesses generated by the program are the total and must be divided by 2 to get the halves of a symmetric laminate. No knowledge of optimization techniques is needed to run the program and very little knowledge of laminate plate theory is needed. In addition, material properties for five common advanced composites are stored in the program, or the computer can ask for new properties through prompts.

Q3dg A Computer Program For Strain Energy Release Rates For Delamination Growth In Composite Laminates

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Author :
language : en
Publisher:
Release Date : 1986

Q3dg A Computer Program For Strain Energy Release Rates For Delamination Growth In Composite Laminates written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with categories.