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pro vyhledávání: '"Roy W. Prowell"'
Autor:
Roy W. Prowell, Ernest K. Gatcombe
Publikováno v:
Journal of Engineering for Industry. 82:223-229
In this paper a rocket motor turbine-pump reduction gear system is analyzed in regard to Hertzian gear tooth contact stresses and times of contact. It is found that the Hertzian contact stresses vary from approximately 100,000 psi to 200,000 psi. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7a87de7117212ab7f259aaf6fa351bc7
https://doi.org/10.1115/1.3663048
https://doi.org/10.1115/1.3663048
