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Effect of radius on bulging and fracture of through-cracked cylindrical pressure vessels at cryogenic temperatures / by Timothy L. Sullivan and William S. Pierce.

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Format:
Book
Government document
Author/Creator:
Sullivan, Timothy L., author.
Pierce, William S. (William Sellers), author.
Contributor:
United States. National Aeronautics and Space Administration, issuing body.
Series:
NASA technical note ; 4951.
NASA TN ; 4951
Language:
English
Subjects (All):
Pressure vessels.
Aluminum alloys.
Titanium alloys.
Fracture mechanics.
aluminum alloy.
Physical Description:
1 online resource (ii, 25 pages) : illustrations.
Place of Publication:
Washington, D.C. : National Aeronautics and Space Administration, December 1968.
Summary:
Burst tests of through-cracked, thin-walled Cylinders fabricated from Ti-5Al-2.5Sn ELI and 2014-T6 Al were conducted at -320 deg and -423 deg F (77 and 20 K). The diameters of the cylinders tested were approximately 6 and 18 in. (15 and 46 cm). The titanium alloy test results showed the pressure bulge coefficient was essentially constant for these two diameters. Comparison of the experimental results with an expression for predicting hoop fracture stress proposed by Eiber showed a good fit with the aluminum alloy data but a poor fit with the titanium alloy data.
Notes:
"December 1968."
Includes bibliographical references (pages 18-19).
Description based on online resource, PDF version; title from title page (NASA, viewed on May 3, 2021).
OCLC:
227934180

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