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Buckling Response of a Large-Scale, Seamless, Orthogrid-Stiffened Metallic CylinderResults 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 characteristics of a seamless cylinder. In addition, the test article and test served as a technology demonstration to show the application of the flow forming manufacturing process to build more efficient buckling-critical structures by eliminating the welded joints that are traditionally used in the manufacturing of large metallic barrels. Pretest predictions of the cylinder buckling response were obtained using a finite-element model that included measured geometric imperfections. The buckling load predicted using this model was 697,000 lb, and the test article buckled at 743,000 lb (6% higher). After the test, the model was revised to account for measured variations in skin and stiffener geometry, nonuniform loading, and material properties. The revised model predicted a buckling load of 754,000 lb, which is within 1.5% of the tested buckling load. In addition, it was determined that the load carrying capability of the seamless cylinder is approximately 28% greater than a corresponding cylinder with welded joints.
Document ID
20180001127
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Rudd, Michelle Tillotson
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hilburger, Mark W.
(NASA Langley Research Center Hampton, VA, United States)
Lovejoy, Andrew E.
(NASA Langley Research Center Hampton, VA, United States)
Lindell, Michael C.
(NASA Langley Research Center Hampton, VA, United States)
Gardner, Nathaniel W.
(Analytic Services and Materials, Inc. Hampton, VA, United States)
Schultz, Marc R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
February 12, 2018
Publication Date
January 8, 2018
Subject Category
Spacecraft Design, Testing And Performance
Launch Vehicles And Launch Operations
Report/Patent Number
M17-6419
Meeting Information
Meeting: AIAA SciTech Forum
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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