Review of Fracture in Adhesive Joints Considering Rocket Motor Application
Abstract
The paper presents a review of existing research on fracture problems in adhesively bonded joints. Both the theoretical background and studies dealing with specific design problems are discussed. Investigations that employed experimental techniques to detect fracture are also included. The work that addresses effects of such important phenomena as residual thermal stresses and viscoelasticity is analyzed. Bond fracture in solid rocket motors is discussed to illustrate an array of problems facing a designer of adhesive joints. Difficulties associated with the analysis of adhesive joints in solid rocket motors are discussed. © 1995 American Institute of Aeronautics and Astronautics, Inc. All right reserved.
Recommended Citation
A. N. Palazotto and V. Birman, "Review of Fracture in Adhesive Joints Considering Rocket Motor Application," Journal of Spacecraft and Rockets, vol. 32, no. 3, pp. 538 - 544, American Institute of Aeronautics and Astronautics, Jan 1995.
The definitive version is available at https://doi.org/10.2514/3.26648
Department(s)
Mechanical and Aerospace Engineering
International Standard Serial Number (ISSN)
0022-4650
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2024 American Institute of Aeronautics and Astronautics, All rights reserved.
Publication Date
01 Jan 1995
