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An experimental study of the strength and stability of thin monocoque shells with reinforced and unreinforced rectangular cutoutsAxial compression tests were run on eleven thin-walled aluminum cylinders having rectangular cutouts. Various types of reinforcement were used around the cutouts, and some tests were run with no reinforcement. The test results are compared with the cylinder buckling loads prior to installation of the cutouts (obtained without damaging the cylinder by using a buckle-capture technique), and correlated with computer-predicted failure loads. The latter were based on the use of the STAGS computer program. For thin cylinders such as these, the test and computer-based analysis shows that for small to moderate size cutouts, reinforcement of the cutout is of no benefit unless the cylinder is of extremely high (geometrical) quality. For cylinder quality and cutout size where reinforcement is beneficial, the relative merits of the various reinforcement configurations are discussed, and an empirical basis for design is proposed.
Document ID
19720006231
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Holmes, A. M. C.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Almroth, B. O.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-115267
LMSC-4-05-71-9
Report Number: NASA-CR-115267
Report Number: LMSC-4-05-71-9
Accession Number
72N13880
Funding Number(s)
CONTRACT_GRANT: NAS9-10372
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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