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Effects of Buckling Knockdown Factor, Internal Pressure and Material on the Design of Stiffened CylindersA design study was conducted to investigate the effect shell buckling knockdown factor (SBKF), internal pressure and aluminum alloy material selection on the structural weight of stiffened cylindrical shells. Two structural optimization codes were used for the design study to determine the optimum minimum-weight design for a series of design cases, and included an in-house developed genetic algorithm (GA) code and PANDA2. Each design case specified a unique set of geometry, material, knockdown factor combinations and loads. The resulting designs were examined and compared to determine the effects of SBKF, internal pressure and material selection on the acreage design weight and controlling failure mode. This design study shows that use of less conservative SBKF values, including internal pressure, and proper selection of material alloy can result in significant weight savings for stiffened cylinders. In particular, buckling-critical cylinders with integrally machined stiffener construction can benefit from the use of thicker plate material that enables taller stiffeners, even when the stiffness, strength and density properties of these materials appear to be inferior.
Document ID
20100016271
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Lovejoy, Andrew E.
(NASA Langley Research Center Hampton, VA, United States)
Hilburger, Mark W.
(NASA Langley Research Center Hampton, VA, United States)
Chunchu, Prasad B.
(Eagle Aeronautics, Inc. Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2010
Subject Category
Structural Mechanics
Report/Patent Number
NF1676L-9232
AIAA Paper-2010-2778
Tracking No. 210774
Report Number: NF1676L-9232
Report Number: AIAA Paper-2010-2778
Report Number: Tracking No. 210774
Meeting Information
Meeting: 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Orlando, FL
Country: United States
Start Date: April 12, 2010
End Date: April 15, 2010
Sponsors: American Society of Civil Engineers, American Society of Mechanical Engineers, American Society for Composites, American Inst. of Aeronautics and Astronautics, American Helicopter Society, Inc.
Funding Number(s)
WBS: WBS 869021.04.07.01.13
Distribution Limits
Public
Copyright
Public Use Permitted.
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