Modified maximum principal stress failure criterion applied to propellant-liner bond failures-Reference-Cited by-同舟云学术

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Modified maximum principal stress failure criterion applied to propellant-liner bond failures

Published:1985-07-08 Issue: Volume: Page:
ISSN:
Container-title:21st Joint Propulsion Conference
language:
Short-container-title:

Author:

KUHLMANN T.¹,PEETERS R.¹,BILLS, JR. K.¹

Affiliation:

1. Aerojet Strategic Propulsion Co., Sacramento, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1439

Reference3 articles.

1. lant-Liner Bonds and Development of Failure Criteria for Ninuteman Wing 11, Second Stage, Propellant-Liner Bond System", Aeroj e t Technical nemorandum, 231, August 1964.

2. Cumulative Damage Program - Final Report", AFRPL-TR-68-131, October 1966.

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1. Stress singularity in a rectangular bond specimen of a solid rocket motor: Effects and elimination;International Journal of Adhesion and Adhesives;2015-12

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