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Use of the EGDA integrator to determine temperature stresses in turbine blades
Matsevityi, I U M
[Place of publication not identified] : [publisher not identified], 1969.
American Institute of Aeronautics and Astronautics. Technical Information Service
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I Want It
Reproduced from: Dinamika I Prochnost' Mashin.
Abstracted in International Aerospace Abstracts.
Microform. New York : American Institute of Aeronautics and Astronautics, Technical Information Service, [19--?]
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| catkey: 20510261