Structural Testing of a Stitched/Resin Film Infused Graphite-Epoxy Wing Box

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Publisher : DIANE Publishing
ISBN 13 : 1428996079
Total Pages : 121 pages
Book Rating : 4.4/5 (289 download)

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Book Synopsis Structural Testing of a Stitched/Resin Film Infused Graphite-Epoxy Wing Box by :

Download or read book Structural Testing of a Stitched/Resin Film Infused Graphite-Epoxy Wing Box written by and published by DIANE Publishing. This book was released on 2001 with total page 121 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Structural Testing of a Stitched/Resin Film Infused Graphite-Epoxy Wing Box

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781721097968
Total Pages : 120 pages
Book Rating : 4.0/5 (979 download)

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Book Synopsis Structural Testing of a Stitched/Resin Film Infused Graphite-Epoxy Wing Box by : National Aeronautics and Space Administration (NASA)

Download or read book Structural Testing of a Stitched/Resin Film Infused Graphite-Epoxy Wing Box written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-15 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of a series of tests conducted at the NASA Langley Research Center to evaluate the behavior of an all-composite full-scale wing box are presented. The wing box is representative of a section of a 220-passenger commercial transport aircraft wing box and was designed and constructed by The Boeing Company as part of the NASA Advanced Subsonics Technology (AST) program. The semi-span wing was fabricated from a graphite-epoxy material system with cover panels and spars held together using Kevlar stitches through the thickness. No mechanical fasteners were used to hold the stiffeners to the skin of the cover panels. Tests were conducted with and without low-speed impact damage, discrete source damage and repairs. Up-bending, down-bending and brake roll loading conditions were applied. The structure with non-visible impact damage carried 97% of Design Ultimate Load prior to failure through a lower cover panel access hole. Jegley, Dawn C. and Bush, Harold G. Langley Research Center RTOP 706-63-71-11

STRUCTURAL TESTING OF A STITCHED/RESIN FILM INFUSED GRAPHITE-EPOXY WING BOX... NASA/TM-2001-210846... JUN. 20, 2001

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (112 download)

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Book Synopsis STRUCTURAL TESTING OF A STITCHED/RESIN FILM INFUSED GRAPHITE-EPOXY WING BOX... NASA/TM-2001-210846... JUN. 20, 2001 by :

Download or read book STRUCTURAL TESTING OF A STITCHED/RESIN FILM INFUSED GRAPHITE-EPOXY WING BOX... NASA/TM-2001-210846... JUN. 20, 2001 written by and published by . This book was released on 2002 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Assessment of the State-of-the-art in the Design and Manufacturing of Large Composite Structures for Aerospace Vehicles

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Publisher :
ISBN 13 :
Total Pages : 182 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis An Assessment of the State-of-the-art in the Design and Manufacturing of Large Composite Structures for Aerospace Vehicles by : Charles E. Harris

Download or read book An Assessment of the State-of-the-art in the Design and Manufacturing of Large Composite Structures for Aerospace Vehicles written by Charles E. Harris and published by . This book was released on 2001 with total page 182 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of an assessment of the state-of-the-art in the design and manufacturing of large composite structures are described. The focus of the assessment is on the use of polymeric matrix composite materials for large airframe structural components, such as those in commercial and military aircraft and space transportation vehicles. Applications of composite materials for large commercial transport aircraft, general aviation aircraft, rotorcraft, military aircraft, and unmanned rocket launch vehicles are reviewed. The results of the assessment of the state-of-the-art include a summary of lessons learned, examples of current practice, and an assessment of advanced technologies under development.

Advanced Durability and Damage Tolerance Design and Analysis Methods for Composite Structures: Lessons Learned from NASA Technology Development Programs

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Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Advanced Durability and Damage Tolerance Design and Analysis Methods for Composite Structures: Lessons Learned from NASA Technology Development Programs by : Charles E. Harris

Download or read book Advanced Durability and Damage Tolerance Design and Analysis Methods for Composite Structures: Lessons Learned from NASA Technology Development Programs written by Charles E. Harris and published by . This book was released on 2003 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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Publisher :
ISBN 13 :
Total Pages : 496 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 2003 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Popular Mechanics

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ISBN 13 :
Total Pages : 138 pages
Book Rating : 4./5 ( download)

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Book Synopsis Popular Mechanics by :

Download or read book Popular Mechanics written by and published by . This book was released on 1995-12 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt: Popular Mechanics inspires, instructs and influences readers to help them master the modern world. Whether it’s practical DIY home-improvement tips, gadgets and digital technology, information on the newest cars or the latest breakthroughs in science -- PM is the ultimate guide to our high-tech lifestyle.

Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722132613
Total Pages : 36 pages
Book Rating : 4.1/5 (326 download)

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Book Synopsis Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box by : National Aeronautics and Space Administration (NASA)

Download or read book Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-02 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The analytical and experimental results of an all-composite wing stub box are presented in this report. The wing stub box, which is representative of an inboard portion of a commercial transport high-aspect-ratio wing, was fabricated from stitched graphite-epoxy material with a Resin Film Infusion manufacturing process. The wing stub box was designed and constructed by the McDonnell Douglas Aerospace Company as part of the NASA Advanced Composites Technology program. The test article contained metallic load-introduction structures on the inboard and outboard ends of the graphite-epoxy wing stub box. The root end of the inboard load introduction structure was attached to a vertical reaction structure, and an upward load was applied to the outermost tip of the outboard load introduction structure to induce bending of the wing stub box. A finite element model was created in which the center portion of the wing-stub-box upper cover panel was modeled with a refined mesh. The refined mesh was required to represent properly the geometrically nonlinear structural behavior of the upper cover panel and to predict accurately the strains in the stringer webs of the stiffened upper cover panel. The analytical and experimental results for deflections and strains are in good agreement. Wang, John T. and Jegley, Dawn C. and Bush, Harold G. and Hinrichs, Stephen C. Langley Research Center RTOP 538-10-11-02...

Popular Mechanics

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Publisher :
ISBN 13 :
Total Pages : 138 pages
Book Rating : 4./5 ( download)

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Book Synopsis Popular Mechanics by :

Download or read book Popular Mechanics written by and published by . This book was released on 1995-12 with total page 138 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box

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Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box by :

Download or read book Correlation of Structural Analysis and Test Results for the McDonnell Douglas Stitched/RFI All-Composite Wing Stub Box written by and published by . This book was released on 1996 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Collection of Technical Papers

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Publisher :
ISBN 13 :
Total Pages : 806 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis A Collection of Technical Papers by :

Download or read book A Collection of Technical Papers written by and published by . This book was released on 2001 with total page 806 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Structural Test Documentation and Results for the McDonnell Douglas All-Composite Wing Stub Box

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Publisher :
ISBN 13 :
Total Pages : 104 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Structural Test Documentation and Results for the McDonnell Douglas All-Composite Wing Stub Box by : Dawn C. Jegley

Download or read book Structural Test Documentation and Results for the McDonnell Douglas All-Composite Wing Stub Box written by Dawn C. Jegley and published by . This book was released on 1997 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Langley Scientific and Technical Information Output-2001

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Publisher :
ISBN 13 :
Total Pages : 166 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis NASA Langley Scientific and Technical Information Output-2001 by :

Download or read book NASA Langley Scientific and Technical Information Output-2001 written by and published by . This book was released on 2002 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Smart Structures and Materials

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Publisher :
ISBN 13 :
Total Pages : 528 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Smart Structures and Materials by :

Download or read book Smart Structures and Materials written by and published by . This book was released on 2001 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Global and Local Stress Analyses of McDonnell Douglas Stitched/RFI Composite Wing Stub Box

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Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Global and Local Stress Analyses of McDonnell Douglas Stitched/RFI Composite Wing Stub Box by : John T. Wang

Download or read book Global and Local Stress Analyses of McDonnell Douglas Stitched/RFI Composite Wing Stub Box written by John T. Wang and published by . This book was released on 1996 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains results of structural analyses performed in support of the NASA structural testing of an all-composite stitched/RFI (resin film infusion) wing stub box. McDonnell Douglas Aerospace Company designed and fabricated the wing stub box. The analyses used a global/local approach. The global model contains the entire test article. It includes the all-composite stub box, a metallic load-transition box and a metallic wing-tip extension box. The two metallic boxes are connected to the inboard and outboard ends of the composite wing stub box, respectively. The load-transition box was attached to a steel and concrete vertical reaction structure and a load was applied at the tip of the extension box to bend the wing stub box upward. The local model contains an upper cover region surrounding three stringer runouts. In that region, a large nonlinear deformation was identified by the global analyses. A more detailed mesh was used for the local model to obtain more accurate analysis results near stringer runouts. Numerous analysis results such as deformed shapes, displacements at selected locations, and strains at critical locations are included in this report.

Development of Stitched, Braided and Woven Composite Structures in the ACT Program and at Langley Research Center

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Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Development of Stitched, Braided and Woven Composite Structures in the ACT Program and at Langley Research Center by : Marvin B. Dow

Download or read book Development of Stitched, Braided and Woven Composite Structures in the ACT Program and at Langley Research Center written by Marvin B. Dow and published by . This book was released on 1997 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Popular Mechanics

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Publisher :
ISBN 13 :
Total Pages : 758 pages
Book Rating : 4.:/5 (318 download)

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Book Synopsis Popular Mechanics by :

Download or read book Popular Mechanics written by and published by . This book was released on 1995 with total page 758 pages. Available in PDF, EPUB and Kindle. Book excerpt: