Zobrazeno 1 - 10 of 54 pro vyhledávání: '"Mark W. Hilburger"'
1
Scaling Methodology Applied to Buckling of Sandwich Composite Cylindrical Shells
Autor: Ines Uriol Balbin, Chiara Bisagni, Marc R. Schultz, Mark W. Hilburger
Publikováno v: AIAA Journal. 58:3680-3689
Studying buckling behavior of large shell structures through full-scale test articles can be complex and expensive. Therefore, reduced-scale structures are often preferred for investigating bucklin...
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::de49663e6f08d5dd4ab6eacb8da1368b
https://doi.org/10.2514/1.j058999
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2
Lessons Learned from Large-Scale Aerospace Structural Testing
Autor: Dawn C. Jegley, Andrew E. Lovejoy, Mark W. Hilburger, Adam Przekop
Publikováno v: AIAA Scitech 2021 Forum.
Large-scale testing of aerospace structures is frequently the final step in a development project to validate the structural performance, and that typically involves a large cost and time investment. In order to ensure that the testing provides the r
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1f67d25c556c7ce09263f57023e95f4b
https://doi.org/10.2514/6.2021-1619
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4
Test and Analysis of Buckling-Critical Stiffened Metallic Launch Vehicle Cylinders
Autor: W. Allen Waters, Nathaniel W. Gardner, Mark W. Hilburger, Michael C. Lindell
Publikováno v: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
A summary of a NASA design analysis and test program on the buckling of large-scale, integrally-stiffened metallic cylinders is presented. The test article designs were developed based on proposed NASA launch vehicle cylinder designs and span a signi
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::09b844637543566a9ea00ac017e29756
https://doi.org/10.2514/6.2018-1697
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5
Test and Analysis of a Buckling-Critical Large-Scale Sandwich Composite Cylinder
Autor: Michelle T. Rudd, Tod Palm, David W. Sleight, Nathan J. Oldfield, Nathaniel W. Gardner, Marc R. Schultz, Mark W. Hilburger
Publikováno v: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Structural stability is an important design consideration for launch-vehicle shell structures and it is well known that the buckling response of such shell structures can be very sensitive to small geometric imperfections. As part of an effort to dev
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::55bc6bb8bede70b68baaa781b4b77f09
https://doi.org/10.2514/6.2018-1693
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6
Buckling Response of a Large-Scale, Seamless, Orthogrid- Stiffened Metallic Cylinder
Autor: Marc R. Schultz, Andrew E. Lovejoy, Michael C. Lindell, Michelle T. Rudd, Nathaniel W. Gardner, Mark W. Hilburger
Publikováno v: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
Results from the buckling test of a compression-loaded 8-ft-diameter seamless (i.e., without manufacturing joints), orthogrid-stiffened metallic cylinder are presented. This test was used to assess the buckling response and imperfection sensitivity c
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::43fb081e112099604747a00d523331eb
https://doi.org/10.2514/6.2018-1987
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8
Test and Analysis of Full-Scale 27.5-Foot-Diameter Stiffened Metallic Launch Vehicle Cylinders
Autor: Nathaniel W. Gardner, Andrew E. Lovejoy, Mark W. Hilburger
Publikováno v: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The Shell Buckling Knockdown Factor Project (SBKF) was established with the goal of developing improved (i.e., less-conservative, more robust) shell buckling knockdown factors (KDFs) for modern launch-vehicle structures. To this end, SBKF has engaged
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f013227324c843c6dbd91bc3ded85c95
https://doi.org/10.2514/6.2018-1989
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9
Implementation of Fiber Optic Sensing System on Sandwich Composite Cylinder Buckling Test
Autor: Allen R. Parker, Francisco Pena, W. Lance Richards, Nathaniel W. Gardner, Michelle T. Rudd, Anthony Piazza, Mark W. Hilburger, Marc R. Schultz
Publikováno v: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The National Aeronautics and Space Administration (NASA) Engineering and Safety Center Shell Buckling Knockdown Factor Project is a multicenter project tasked with developing new analysis-based shell buckling design guidelines and design factors (i.e
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::aff88395e08e2e5674ce0c28ff037d82
https://doi.org/10.2514/6.2018-1695
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10
Digital Image Correlation Data Processing and Analysis Techniques to Enhance Test Data Assessment and Improve Structural Simulations
Autor: Nathaniel W. Gardner, Mark W. Hilburger, Waddy T. Haynie, Michael C. Lindell, W. Allen Waters
Publikováno v: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The NASA Shell Buckling Knockdown Factor Project (SBKF) was established in 2007 by the NASA Engineering and Safety Center (NESC) with the primary goal to develop new analysis-based buckling design factors (a.k.a. knockdown factors) and high-fidelity
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::a62e8ac1df849cd85675c45c6ef467ec
https://doi.org/10.2514/6.2018-1698
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