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Determination of the deformations of a thick- walled cylinder connected to a rigid chamber in the case of a physically nonlinear elasticity law applied to a solid fuel booster
Author
Burmistrov, V P.
Published
[Place of publication not identified] : [publisher not identified], 1968.
Physical Description
pages 153-157
Additional Creators
American Institute of Aeronautics and Astronautics. Technical Information Service
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Language Note
In Russian.
Subject(s)
Aeronautics
Collection
IAA papers.
Note
A69-25347.
Abstracted in International Aerospace Abstracts.
Reproduced from: Aviatsionnaia Tekhnika
Reproduction Note
Microform. New York : American Institute of Aeronautics and Astronautics, Technical Information Service, [19--?]
View MARC record
| catkey: 19133742